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  • Inorganic Chemistry  (1,406)
  • Acoustics
  • 1995-1999  (58)
  • 1990-1994  (734)
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  • 1935-1939  (675)
  • 1998  (58)
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  • 1995-1999  (58)
  • 1990-1994  (734)
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  • 1
    Electronic Resource
    Electronic Resource
    Springer
    Journal of comparative physiology 183 (1998), S. 513-518 
    ISSN: 1432-1351
    Keywords: Key words Cerci ; Multimodal ; Near-field ; Acoustics ; Communication
    Source: Springer Online Journal Archives 1860-2000
    Topics: Biology , Medicine
    Notes: Abstract Wing movements associated with stridulation by the male during cricket courtship generate air movements that have been proposed to serve as signals to the female. We assessed this putative signaling role by interfering with the presumed communications channel in two ways: (1) by removing the female's cerci, which are candidate sensory organs for signal reception, and (2) by trimming the male's forewings and thus manipulating the signal itself. We measured the effects of these treatments on the probability and latency with which females mounted courting males. We found that neither treatment affected female mounting behavior. This was true both for old, highly motivated females and for younger females, which are less highly motivated and possibly more selective. We conclude that air movements play little or no role as signals that release female mounting behavior during courtship.
    Type of Medium: Electronic Resource
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  • 2
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    In:  DGG-Mittl., Münster, 3, vol. 75, no. 2, pp. 2-32, pp. L12311, (ISBN 0-471-26610-8)
    Publication Date: 1998
    Keywords: Deep seismic sounding (espec. cont. crust) ; Refraction seismics ; Reflection seismics ; Acoustics ; Travel time ; Earth model, also for more shallow analyses ! ; Velocity depth profile
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  • 3
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    In:  Geophys. J. Int., Amsterdam, Schweizerbart'sche Verlagsbuchhandlung, vol. 135, no. 3, pp. 999-1010, pp. L12S09, (ISSN 0016-8548, ISBN 3-510-50045-8)
    Publication Date: 1998
    Keywords: Randomly layered ; Reflection seismics ; Travel time ; Wave propagation ; Anisotropy ; Inversion ; Acoustics ; GJI
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  • 4
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    In:  Phys. Earth Plan. Int., Hannover, Polish Geothermal Association, vol. 108, no. 2, pp. 103-114, pp. 1051, (ISSN: 1340-4202)
    Publication Date: 1998
    Keywords: Crustal deformation (cf. Earthquake precursor: deformation or strain) ; Geodesy ; ocean ; Plate tectonics ; Seismicity ; Acoustics ; PEPI
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  • 5
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    Elsevier
    In:  Amsterdam, Elsevier, vol. 1, no. ALEX(01)-FR-77-01, AFTAC Contract F08606-76-C-0025, pp. 95-104, (ISBN 1-85312-745-0)
    Publication Date: 1998
    Keywords: Inversion ; Elasticity ; Geothermics ; Scattering ; soil ; Modelling ; Fluids ; Acoustics
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  • 6
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    Elsevier
    In:  Amsterdam, Elsevier, vol. 47, no. 22, pp. 65-70, (ISBN 3-7643-0253-4)
    Publication Date: 1998
    Keywords: Modelling ; Finite Element Method ; Elasticity ; Error analysis ; Acoustics
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  • 7
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    Hydrographic Department, Maritime Safety Agency
    In:  report, 9 pp., Tokyo, Hydrographic Department, Maritime Safety Agency, vol. C 560, 183 pp., no. PL-TR-92-2005, pp. 106-117, (ISBN 3-933346-037)
    Publication Date: 1998
    Keywords: Crustal deformation (cf. Earthquake precursor: deformation or strain) ; ocean ; seafloor ; Global Positioning System ; SAR ; Acoustics
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  • 8
    Publication Date: 2013-08-31
    Description: The primary objective of our work was to evaluate and test several wake management schemes for the reduction of turbomachinery fan noise. Throughout the course of this work we relied on several tools. These include 1) Two-dimensional steady boundary-layer and wake analyses using MISES (a thin-shear layer Navier-Stokes code), 2) Two-dimensional unsteady wake-stator interaction simulations using UNSFLO, 3) Three-dimensional, steady Navier-Stokes rotor simulations using NEWT, 4) Internal blade passage design using quasi-one-dimensional passage flow models developed at MIT, 5) Acoustic modeling using LINSUB, 6) Acoustic modeling using VO72, 7) Experiments in a low-speed cascade wind-tunnel, and 8) ADP fan rig tests in the MIT Blowdown Compressor.
    Keywords: Acoustics
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  • 9
    Publication Date: 2011-08-23
    Description: A Navier-Stokes computer code is used to predict one of the ducted-fan engine acoustic modes that results from rotor-wake/stator-blade interaction. A patched sliding-zone interface is employed to pass information between the moving rotor row and the stationary stator row. The code produces averaged aerodynamic results downstream of the rotor that agree well with a widely used average-passage code. The acoustic mode of interest is generated successfully by the code and is propagated well upstream of the rotor, temporal and spatial numerical resolution are fine enough such that attenuation of the signal is small. Two acoustic codes are used to find the far-field noise. Near-field propagation is computed by using Eversman's wave envelope code, which is based on a finite-element model. Propagation to the far field is accomplished by using the Kirchhoff formula for moving surfaces with the results of the wave envelope code as input data. Comparison of measured and computed far-field noise levels show fair agreement in the range of directivity angles where the peak radiation lobes from the inlet are observed. Although only a single acoustic mode is targeted in this study, the main conclusion is a proof-of-concept: Navier Stokes codes can be used both to generate and propagate rotor-stator acoustic modes forward through an engine, where the results can be coupled to other far-field noise prediction codes.
    Keywords: Acoustics
    Type: Journal of Sound and Vibration (ISSN 0022-460X); Volume 213; No. 4; 643-664
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  • 10
    Publication Date: 2011-08-23
    Description: In this paper, predictions are made of noise radiation from single, supersonic, axisymmetric jets. We examine the effects of changes in operating conditions and the effects of simulated enhanced mixing that would increase the spreading rate of jet shear layer on radiated noise levels. The radiated noise in the downstream direction is dominated by mixing noise and, at higher speeds, it is well described by the instability wave noise radiation model. Further analysis with the model shows a relationship between changes in spreading rate due to enhanced mixing and changes in the far field radiated peak noise levels. The calculations predict that enhanced jet spreading results in a reduction of the radiated peak noise level.
    Keywords: Acoustics
    Type: Journal of Fluids Engineering; Volume 120; 471-476
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  • 11
    Publication Date: 2011-08-23
    Description: An algorithm for generating appropriate velocity boundary conditions for an acoustic boundary element analysis from the kinematics of an operating propeller is presented. It constitutes the initial phase of Integrating sophisticated rotorcraft models into a conventional boundary element analysis. Currently, the pressure field is computed by a linear approximation. An initial validation of the developed process was performed by comparing numerical results to test data for the external acoustic pressure on the surface of a tilt-rotor aircraft for one flight condition.
    Keywords: Acoustics
    Type: Noise Control Engineering; Volume 46; No. 3; 132-136
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  • 12
    Publication Date: 2018-06-05
    Description: A comparison was made between two approaches to predict acoustic emission waveforms in thin plates. A normal mode solution method for Mindlin plate theory was used to predict the response of the flexural plate mode to a point source, step-function load, applied on the plate surface. The second approach used a dynamic finite element method to model the problem using equations of motion based on exact linear elasticity. Calculations were made using properties for both isotropic (aluminum) and anisotropic (unidirectional graphite/epoxy composite) materials. For simulations of anisotropic plates, propagation along multiple directions was evaluated. In general, agreement between the two theoretical approaches was good. Discrepancies in the waveforms at longer times were caused by differences in reflections from the lateral plate boundaries. These differences resulted from the fact that the two methods used different boundary conditions. At shorter times in the signals, before reflections, the slight discrepancies in the waveforms were attributed to limitations of Mindlin plate theory, which is an approximate plate theory. The advantages of the finite element method are that it used the exact linear elasticity solutions, and that it can be used to model real source conditions and complicated, finite specimen geometries as well as thick plates. These advantages come at a cost of increased computational difficulty, requiring lengthy calculations on workstations or supercomputers. The Mindlin plate theory solutions, meanwhile, can be quickly generated on personal computers. Specimens with finite geometry can also be modeled. However, only limited simple geometries such as circular or rectangular plates can easily be accommodated with the normal mode solution technique. Likewise, very limited source configurations can be modeled and plate theory is applicable only to thin plates.
    Keywords: Acoustics
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  • 13
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    In:  CASI
    Publication Date: 2019-06-28
    Description: Test procedures related to XV-15 noise tests conducted by NASA-Langley and Bell Helicopter Textron, Inc. are discussed. The tests. which took place during October and November 1995, near Waxahachie, Texas, documented the noise signature of the XV-15 tilt-rotor aircraft at a wide variety of flight conditions. The stated objectives were to: -provide a comprehensive acoustic database for NASA and U.S. Industry -validate noise prediction methodologies, and -develop and demonstrate low-noise flight profiles. The test consisted of two distinct phases. Phase 1 provided an acoustic database for validating analytical noise prediction techniques; Phase 2 directly measured noise contour information at a broad range of operating profiles, with emphasis on minimizing 'approach' noise. This report is limited to a documentation of the test procedures, flight conditions, microphone locations, meteorological conditions, and test personnel used in the test. The acoustic results are not included.
    Keywords: Acoustics
    Type: NASA/CR-1998-206946 , NAS 1.26:206946 , BHTI-690-099-450
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  • 14
    Publication Date: 2019-06-28
    Description: An innovative hyperbolic preconditioning technique is developed for the numerical solution of the Helmholtz equation which governs acoustic propagation in ducts. Two pseudo-time parameters are used to produce an explicit iterative finite difference scheme. This scheme eliminates the large matrix storage requirements normally associated with numerical solutions to the Helmholtz equation. The solution procedure is very fast when compared to other transient and steady methods. Optimization and an error analysis of the preconditioning factors are present. For validation, the method is applied to sound propagation in a 2D semi-infinite hard wall duct.
    Keywords: Acoustics
    Type: NASA/TM-107349 , NAS 1.15:107349 , E-10501
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  • 15
    Publication Date: 2019-06-28
    Description: A system for detecting ultrasonic vibrations. such as those generated by a small leak in a pressurized container. vessel. pipe. or the like. comprises an ultrasonic transducer assembly and a processing circuit for converting transducer signals into an audio frequency range signal. The audio frequency range signal can be used to drive a pair of headphones worn by an operator. A diode rectifier based mixing circuit provides a simple, inexpensive way to mix the transducer signal with a square wave signal generated by an oscillator, and thereby generate the audio frequency signal. The sensitivity of the system is greatly increased through proper selection and matching of the system components. and the use of noise rejection filters and elements. In addition, a parabolic collecting horn is preferably employed which is mounted on the transducer assembly housing. The collecting horn increases sensitivity of the system by amplifying the received signals. and provides directionality which facilitates easier location of an ultrasonic vibration source.
    Keywords: Acoustics
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  • 16
    Publication Date: 2018-06-02
    Description: The proposed U.S. High Speed Civil Transport (HSCT) will revolutionize commercial air travel by providing economical supersonic passenger service to destinations worldwide. Unlike the high-bypass turbofan engines that propel today's subsonic airliners, HSCT engines will have much higher jet exhaust speeds. Jet noise, caused by the turbulent mixing of high-speed exhaust with the surrounding air, poses a significant challenge for HSCT engine designers. To resolve this challenge, engineers have designed advanced mixer rejector nozzles that reduce HSCT jet noise to airport noise certification levels by entraining and mixing large quantities of ambient air with the engines' jet streams. Although this works well during the first several minutes of flight, far away from the airport, as the HSCT gains speed and climbs, poor ejector inlet recovery and ejector ram drag contribute to poor thrust, making it advantageous to turn off the ejector. Doing so prematurely, however, can cause unacceptable noise levels to propagate to the ground, even when the aircraft is many miles from the airport. This situation lends itself ideally to optimization, where the aircraft trajectory, throttle setting, and ejector setting can be varied (subject to practical aircraft constraints) to minimize the noise propagated to the ground. A method was developed at the NASA Lewis Research Center that employs a variation of the classic energy state approximation: a trajectory analysis technique historically used to minimize climb time or fuel burned in many aircraft problems. To minimize the noise on the ground at any given throttle setting, high aircraft altitudes are desirable; but the HSCT may either climb quickly to high altitudes using a high, noisy throttle setting or climb more slowly at a lower, quieter throttle setting. An optimizer has been programmed into NASA's existing aircraft and noise analysis codes to balance these options by dynamically choosing the best altitude-velocity path and throttle setting history. The noise level standard, or metric, used in the optimizer should be one that accurately reflects the subjective annoyance levels of ground-based observers under the flight path. A variety of noise metrics are available, many of which are practical for airport-vicinity noise certification. Unlike airport noise, however, the HSCT's climb noise will be characterized by relatively low noise levels, long durations, and low-frequency spectra. The noise metrics used in these calculations are based on the recommendations of researchers at the NASA Langley Research Center, who have correlated the flyover noise annoyance levels of actual laboratory subjects with a variety of measurements. Analysis of data from this optimizer has shown that significant reductions in noise may be obtained with trajectory optimization. And since throttling operations are performed in the subsonic portion of the climb path (where thrust is plentiful), only small penalties in HSCT range or fuel performance occur.
    Keywords: Acoustics
    Type: Research and Technology 1997; NASA/TM-1998-206312
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  • 17
    Publication Date: 2019-06-28
    Description: This report describes the development of prediction methods for broadband fan noise from aircraft engines. First, experimental evidence of the most important source mechanisms is reviewed. It is found that there are a number of competing source mechanism involved and that there is no single dominant source to which noise control procedures can be applied. Theoretical models are then developed for: (1) ducted rotors and stator vanes interacting with duct wall boundary layers, (2) ducted rotor self noise, and (3) stator vanes operating in the wakes of rotors. All the turbulence parameters required for these models are based on measured quantities. Finally the theoretical models are used to predict measured fan noise levels with some success.
    Keywords: Acoustics
    Type: NASA/CR-1998-207752 , NAS 1.26:207752
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  • 18
    Publication Date: 2019-07-18
    Description: Engineering constraints that may be encountered when implementing interactive virtual acoustic displays are examined In particular, system parameters such as the update rate and total system latency are defined and the impact they may have on perception is discussed. For example, examination of the head motions that listeners used to aid localization in a previous study suggests that some head motions may be as fast as about 400 degrees/sec for short time periods. Analysis of latencies in virtual acoustic environments (VAEs) suggests that: (1) commonly-specified parameters such as the audio update rate determine only the "best-case" latency possible in a VAE, (2) total system latency and individual latencies of system components, including head-trackers, are frequently not measured by VAE developers, and (3) typical system latencies may result in under-sampling of relative listener-source motion of 400 degrees/sec as well as positional "jitter" in the simulated source. To clearly specify the dynamic performance of a particular VAE, users and developers need to make measurements of average system latency, update rate, and their variability using standardized rendering scenarios. a parameters such as the minimum audible movement angle can then be used as target guidelines to assess whether a given system meets perceptual requirements.
    Keywords: Acoustics
    Type: Acoustical Society of America Conference; Jun 20, 1998 - Jun 28, 1998; Seattle, WA; United States
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  • 19
    Publication Date: 2019-07-18
    Description: Auditory thresholds for 10 subjects were obtained for speech stimuli reverberation. The reverberation was produced and manipulated by 3-D audio modeling based on an actual room. The independent variables were octave-band-filtering (bypassed, 0.25 - 2.0 kHz Fc) and reverberation time (0.2- 1.1 sec). An ANOVA revealed significant effects (threshold range: -19 to -35 dB re 60 dB SRL).
    Keywords: Acoustics
    Type: Audio Engineering Society Meeting 104th Conference; May 16, 1998 - May 19, 1998; Amsterdam; Netherlands
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  • 20
    Publication Date: 2019-07-13
    Description: In this paper we demonstrate the usefulness of the ducted fan noise prediction code TBIEM3D as a liner optimization design tool. Boundary conditions on the interior duct wall allow for hard walls or a locally reacting liner with axially segmented, circumferentially uniform impedance. Two liner optimization studies are considered in which farfield noise attenuation due to the presence of a liner is maximized by adjusting the liner impedance. In the first example, the dependence of optimal liner impedance on frequency and liner length is examined. Results show that both the optimal impedance and attenuation levels are significantly influenced by liner length and frequency. In the second example, TBIEM3D is used to compare radiated sound pressure levels between optimal and non-optimal liner cases at conditions designed to simulate take-off. It is shown that significant noise reduction is achieved for most of the sound field by selecting the optimal or near optimal liner impedance. Our results also indicate that there is relatively large region of the impedance plane over which optimal or near optimal liner behavior is attainable. This is an important conclusion for the designer since there are variations in liner characteristics due to manufacturing imprecisions.
    Keywords: Acoustics
    Type: AIAA Paper 98-2310 , 4th AIAA/CEAS Aeroacoustics Conference; Jun 02, 1998 - Jun 04, 1998; Toulouse; France
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  • 21
    Publication Date: 2019-07-13
    Description: In recent work, a microphone array consisting of an omnidirectional microphone and colocated dipole microphones having orthogonally aligned dipole axes was used to examine the directional nature of a room impulse response. The arrival of significant reflections was indicated by peaks in the power of the omnidirectional microphone response; reflection direction of arrival was revealed by comparing zero-lag crosscorrelations between the omnidirectional response and the dipole responses to the omnidirectional response power to estimate arrival direction cosines with respect to the dipole axes.
    Keywords: Acoustics
    Type: 1998 Int. Congress Noise Control Engineering; Nov 16, 1998 - Nov 18, 1998; Christchurch; New Zealand
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  • 22
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    In:  CASI
    Publication Date: 2019-07-13
    Description: The Aeroacoustics Research Program is an integral part of the Joint Institute for Advancement of Flight Sciences at The George Washington University. It is affiliated with many civil, mechanical, and environmental engineering courses, particularly those that stress theory and numerical or other analytic methods in engineering. This report lists the courses presented, the names of graduate research assistants, and bibliographic information regarding publications and presentations. Three graduate degrees were awarded and the abstracts of each dissertation is included. The dissertations were as follows: "A Numerical Investigation of Thermoacoustic Oscillations", which discusses advances in the study of acoustic phenomena through the use of computational aeroacoustics. "Computation of Vortex Shedding and Radiated Sound for a Circular Cylinder: Subcritical to Transcritical Reynolds Numbers", which discusses predicting tonal noise generated by vortex shedding from a circular cylinder. And finally, "The Radiated Field Generated by a Monopole Source in a Short, Rigid, Rectangular Duct", which develops a method for modeling the acoustic field generated by a monopole source placed in a moving rectangular duct.
    Keywords: Acoustics
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  • 23
    Publication Date: 2019-07-13
    Description: An advanced high bypass ratio fan model was tested in the NASA Lewis Research Center 9 x 15-Foot Low Speed Wind Tunnel. The primary focus of this test was to quantify the acoustic benefits and aerodynamic performance of sweep and lean in stator vane design. Three stator sets were used for this test series. A conventional radial stator was tested at two rotor-stator axial spacings. Additional stator sets incorporating sweep + lean, and sweep only were also tested. The hub axial location for the swept + lean, and sweep only stators corresponded to the location of the radial stator at the upstream rotor-stator spacing, while the tip axial location of these modified stators corresponded to the radial stator axial position at the downstream position. The acoustic results show significant reductions in both rotor-stator interaction noise and broadband noise beyond what could be achieved through increased axial spacing of the conventional, radial stator. Theoretical application of these results to acoustically quantify a fictitious 2-engine aircraft and flight path suggested that about 3 Effective Perceived Noise (EPN) dB could be achieved through incorporation of these modified stators. This reduction would represent a significant portion of the 6 EPNdB noise goal of the current NASA Advanced Subsonic Technology (AST) initiative relative to that of 1992 technology levels. A secondary result of this fan test was to demonstrate the ability of an acoustic barrier wall to block aft-radiated fan noise in the wind tunnel, thus revealing the acoustic structure of the residual inlet-radiated noise. This technology should prove valuable toward better understanding inlet liner design, or wherever it is desirable to eliminate aft-radiated noise from the fan acoustic signature.
    Keywords: Acoustics
    Type: NASA/TM-1998-208661 , NAS 1.15:208661 , AIAA Paper 99-0479 , E-11382 , Aerospace Sciences Meeting and Exhibit; Jan 11, 1999 - Jan 14, 1999; Reno, NV; United States
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  • 24
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    In:  CASI
    Publication Date: 2019-07-13
    Description: Closed form asymptotic expressions for computing high frequency noise generated by an annular cascade in an infinite duct containing a uniform flow are presented. There are two new elements in this work. First, the annular duct mode representation does not rely on the often-used Bessel function expansion resulting in simpler expressions for both the radial eigenvalues and eigenfunctions of the duct. In particular, the new representation provides an explicit approximate formula for the radial eigenvalues obviating the need for solutions of the transcendental annular duct eigenvalue equation. Also, the radial eigenfunctions are represented in terms of exponentials eliminating the numerical problems associated with generating the Bessel functions on a computer. The second new element is the construction of an unsteady response model for an annular cascade. The new construction satisfies the boundary conditions on both the cascade and duct walls simultaneously adding a new level of realism to the noise calculations. Preliminary results which demonstrate the effectiveness of the new elements are presented. A discussion of the utility of the asymptotic formulas for calculating cascade discrete tone as well as broadband noise is also included.
    Keywords: Acoustics
    Type: NASA/TM-1998-208495 , NAS 1.15:208495 , E-11289 , AIAA Paper 98-2318 , Aeroacoustics Conference; Jun 02, 1998 - Jun 04, 1998; Toulouse; France
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  • 25
    Publication Date: 2019-07-13
    Description: An overview of the development of two microphone directional arrays for aeroacoustic testing is presented. These arrays were specifically developed to measure airframe noise in the NASA Langley Quiet Flow Facility. A large aperture directional array using 35 flush-mounted microphones was constructed to obtain high resolution noise localization maps around airframe models. This array possesses a maximum diagonal aperture size of 34 inches. A unique logarithmic spiral layout design was chosen for the targeted frequency range of 2-30 kHz. Complementing the large array is a small aperture directional array, constructed to obtain spectra and directivity information from regions on the model. This array, possessing 33 microphones with a maximum diagonal aperture size of 7.76 inches, is easily moved about the model in elevation and azimuth. Custom microphone shading algorithms have been developed to provide a frequency- and position-invariant sensing area from 10-40 kHz with an overall targeted frequency range for the array of 5-60 kHz. Both arrays are employed in acoustic measurements of a 6 percent of full scale airframe model consisting of a main element NACA 632-215 wing section with a 30 percent chord half-span flap. Representative data obtained from these measurements is presented, along with details of the array calibration and data post-processing procedures.
    Keywords: Acoustics
    Type: NASA/TM-1998-207321 , NAS 1.15:207321 , AIAA Paper 98-0471 , Aerospace Sciences Meeting and Exhibit; Jan 12, 1998 - Jan 15, 1998; Reno, NV; United States
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  • 26
    Publication Date: 2019-07-18
    Description: When making noise measurements of sound sources in flow using microphones immersed in an air stream or wind tunnel, the factor limiting the dynamic range of the measurement is, in many cases, the noise caused by the flow over the microphone. To lower this self-noise, and to protect the microphone diaphragm, an aerodynamic microphone forebody is usually mounted on the tip of the omnidirectional microphone. The microphone probe is then pointed into the wind stream. Even with a microphone forebody, however, the self-noise persists, prompting further research in the area of microphone forebody design for flow-induced self-noise reduction. The magnitude and frequency characteristics of in-flow microphone probe self-noise is dependent upon the exterior shape of the probe and on the level of turbulence in the onset flow, among other things. Several recent studies present new designs for microphone forebodies, some showing the forbodies' self-noise characteristics when used in a given facility. However, these self-noise characteristics may change when the probes are used in different facilities. The present paper will present results of an experimental investigation to determine an empirical relationship between flow turbulence and self-noise levels for several microphone forebody shapes as a function of frequency. As a result, the microphone probe self-noise for these probes will be known as a function of freestream turbulence, and knowing the freestream turbulence spectra for a given facility, the probe self-noise can be predicted. Flow-induced microphone self-noise is believed to be related to the freestream. turbulence by three separate mechanisms. The first mechanism is produced by large scale, as compared to the probe size, turbulence which appears to the probe as a variation in the angle of attack of the freestream. flow. This apparent angle of attack variation causes the pressure along the probe surface to fluctuate, and at the location of the sensor orifice this fluctuating surface pressure is sensed by the diaphragm as noise. The second mechanism is caused by the convection of smaller sized turbulence, on the order of the probe cross-section, which passes nearby or strikes the probe giving rise to a fluctuating pressure at the sensor orifice. And, the third mechanism is related to fine scale turbulence through its effects on boundary layer growth and transition to a turbulent boundary layer. The method for relating the probe self-noise to the freestream turbulence will be based on the method of K. J. Young5 from Boeing, who developed the technique and presented flow noise results for a Bruel & Kjaer Type 0385, 1/4 inch (6.35 mm) nose cone. The experimental set-up used in the present experiment is similar to that of Young and is described in the present paper. Finally, flow noise predictions are made using the empirical correlations. These predictions are then compared with actual flow noise measurements made in the National Full-Scale Aerodynamics Complex 40- by 80-Foot Wind Tunnel at NASA Ames Research Center.
    Keywords: Acoustics
    Type: 1998 AIAA/CEAS Joint Acoustics Conference; Jun 02, 1998 - Jun 04, 1998; Toulouse; France
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  • 27
    Publication Date: 2019-07-18
    Description: Virtual acoustics, also known as 3-D sound and auralization, is the simulation of the complex acoustic field experienced by a listener within an environment. Going beyond the simple intensity panning of normal stereo techniques, the goal is to process sounds so that they appear to come from particular locations in three-dimensional space. Although loudspeaker systems are being developed, most of the recent work focuses on using headphones for playback and is the outgrowth of earlier analog techniques. For example, in binaural recording, the sound of an orchestra playing classical music is recorded through small mics in the two "ear canals" of an anthropomorphic artificial or "dummy" head placed in the audience of a concert hall. When the recorded piece is played back over headphones, the listener passively experiences the illusion of hearing the violins on the left and the cellos on the right, along with all the associated echoes, resonances, and ambience of the original environment. Current techniques use digital signal processing to synthesize the acoustical properties that people use to localize a sound source in space. Thus, they provide the flexibility of a kind of digital dummy head, allowing a more active experience in which a listener can both design and move around or interact with a simulated acoustic environment in real time. Such simulations are being developed for a variety of application areas including architectural acoustics, advanced human-computer interfaces, telepresence and virtual reality, navigation aids for the visually-impaired, and as a test bed for psychoacoustical investigations of complex spatial cues. The tutorial will review the basic psychoacoustical cues that determine human sound localization and the techniques used to measure these cues as Head-Related Transfer Functions (HRTFs) for the purpose of synthesizing virtual acoustic environments. The only conclusive test of the adequacy of such simulations is an operational one in which the localization of real and synthesized stimuli are directly compared in psychophysical studies. To this end, the results of psychophysical experiments examining the perceptual validity of the synthesis technique will be reviewed and factors that can enhance perceptual accuracy and realism will be discussed. Of particular interest is the relationship between individual differences in HRTFs and in behavior, the role of reverberant cues in reducing the perceptual errors observed with virtual sound sources, and the importance of developing perceptually valid methods of simplifying the synthesis technique. Recent attempts to implement the synthesis technique in real time systems will also be discussed and an attempt made to interpret their quoted system specifications in terms of perceptual performance. Finally, some critical research and technology development issues for the future will be outlined.
    Keywords: Acoustics
    Type: ICAD ''98 International Conference on Auditory Display; Nov 01, 1998 - Nov 04, 1998; Glasgow, Scotland; United Kingdom
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  • 28
    Publication Date: 2019-08-15
    Description: This report describes a theoretical design and analysis study of the benefits of vane sweep and lean for reducing rotor- stator interaction tone noise. It is shown that the kinematic relationship between the rotor wakes and stator vanes is the principal factor in determining the achievable noise reductions. Vane sweep and lean control rotor wake skewing as seen by the stator vanes and hence influence the number of wake intersections per vane. An increase in the number of intersections reduces noise levels. Hence, to reduce rotor-stator noise, van sweep and lean must be chosen in such a way as to increase wake intersections per vane. A simple design rule is thus proposed which requires a sweep configuration that puts the vane tip downstream of its root and a vane lean that is in the direction of the rotor rotation. A detailed comparison of the predicted and measured noise reductions for a swept and leaned stator is then carried out. Overall, these comparisons show that the predicted benefits of a swept and leaned stator are in good agreement, qualitative as well as quantitative, with the measured reductions for the fan speeds relevant to noise certification procedure. Furthermore, the results also demonstrate the validity of design criterion and the theoretical tools used in this study.
    Keywords: Acoustics
    Type: NASA/TM-1998-208662 , NAS 1.15:208662 , E-11383
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  • 29
    Publication Date: 2019-07-10
    Description: The measurement of pure tone acoustic pressure signals in the presence of masking noise, often generated by mean flow, is a continual problem in the field of passive liner duct acoustics research. In support of the Advanced Subsonic Technology Noise Reduction Program, methods were investigated for conducting measurements of advanced duct liner concepts in harsh, aeroacoustic environments. This report presents the results of a comparison study of three signal extraction methods for acquiring quality acoustic pressure measurements in the presence of broadband noise (used to simulate the effects of mean flow). The performance of each method was compared to a baseline measurement of a pure tone acoustic pressure 3 dB above a uniform, broadband noise background.
    Keywords: Acoustics
    Type: NASA/TM-1998-208426 , NAS 1.15:208426 , L-17736
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  • 30
    Publication Date: 2019-07-10
    Description: This study assessed the feasibility of using complaint information archived by modem airport monitoring systems to conduct quantitative analyses of the causes of aircraft noise complaints and their relationship to noise- induced annoyance. It was found that all computer-based airport monitoring systems provide at least rudimentary tools for performing data base searches by complainant name, address, date, time of day, and types of aircraft and complaints. Analyses of such information can provide useful information about longstanding concerns, such as the extent to which complaint rates are driven by objectively measurable aspects of aircraft operations; the degree to which changes in complaint rates can be predicted prior to implementation of noise mitigation measures; and the degree to which aircraft complaint information can be used to simplify and otherwise improve prediction of the prevalence of noise-induced annoyance in communities.
    Keywords: Acoustics
    Type: NASA/CR-1998-207650 , NAS 1.26:207650 , BBN-8215
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  • 31
    Publication Date: 2019-07-10
    Description: As fan tip speeds are reduced, broadband noise is becoming more important in the calculation of perceived noise. Past experience indicates that lower vane number stators with either constant chord or constant solidity may be a way to reduce broadband noise caused by the interaction of the rotor wake turbulence with the stators. A baseline fan and a low blade number fan were investigated to determine if a noise reduction was possible. The low vane number fan showed a 2 PndB and a 1.5 PNLT noise reduction. These reductions show that this is a viable technique for reducing the perceived noise of low tip speed fans.
    Keywords: Acoustics
    Type: NASA/TM-1998-206627 , NAS 1.15:206627 , E-11071
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  • 32
    Publication Date: 2019-07-10
    Description: This document details the methodology and use of the CAMRAD.Mod1/HIRES codes, which were developed at NASA Langley Research Center for the prediction of helicopter harmonic and Blade-Vortex Interaction (BVI) noise. CANMAD.Mod1 is a substantially modified version of the performance/trim/wake code CANMAD. High resolution blade loading is determined in post-processing by HIRES and an associated indicial aerodynamics code. Extensive capabilities of importance to noise prediction accuracy are documented, including a new multi-core tip vortex roll-up wake model, higher harmonic and individual blade control, tunnel and fuselage correction input, diagnostic blade motion input, and interfaces for acoustic and CFD aerodynamics codes. Modifications and new code capabilities are documented with examples. A users' job preparation guide and listings of variables and namelists are given.
    Keywords: Acoustics
    Type: NASA/TM-1998-207640 , L-17697 , NAS 1.26:207640
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  • 33
    Publication Date: 2019-07-10
    Description: This work addresses the design and application of robust controllers for structural acoustic control. Both simulation and experimental results are presented. H(infinity) and mu-synthesis design methods were used to design feedback controllers which minimize power radiated from a panel while avoiding instability due to unmodeled dynamics. Specifically, high order structural modes which couple strongly to the actuator-sensor path were poorly modeled. This model error was analytically bounded with an uncertainty model, which allowed controllers to be designed without artificial limits on control effort. It is found that robust control methods provide the control designer with physically meaningful parameters with which to tune control designs and can be very useful in determining limits of performance. Experimental results also showed, however, poor robustness properties for control designs with ad-hoc uncertainty models. The importance of quantifying and bounding model errors is discussed.
    Keywords: Acoustics
    Type: AIAA Paper 98-2089
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  • 34
    Publication Date: 2019-08-28
    Description: A method and system are provided to detect defects in a material. Waves of known frequency(ies) are mixed at an interaction zone in the material. As a result, at least one of a difference wave and a sum wave are generated in the interaction zone. The difference wave occurs at a difference frequency and the sum wave occurs at a sum frequency. The amplitude of at least one nonlinear signal based on the sum and/or difference waves is then measured. The nonlinear signal is defined as the amplitude of one of the difference wave and sum wave relative to the product of the amplitude of the surface waves. The amplitude of the nonlinear signal is an indication of defects (e.g., dislocation dipole density) in the interaction zone.
    Keywords: Acoustics
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  • 35
    Publication Date: 2019-07-10
    Description: A self-calibrating, remote programmable signal conditioning amplifier system employs information read from a memory attached to a measurement transducer for automatic calibration. The signal conditioning amplifier is self-calibrated on a continuous basis through use of a dual input path arrangement, with each path containing a multiplexer and a programmable amplifier. A digital signal processor controls operation of the system such that a transducer signal is applied to one of the input paths, while one or more calibration signals are applied to the second input path. Once the second path is calibrated, the digital signal processor switches the transducer signal to the second path. and then calibrates the first path. This process is continually repeated so that each path is calibrated on an essentially continuous basis. Dual output paths are also employed which are calibrated in the same manner. The digital signal processor also allows the implementation of a variety of digital filters which are either programmed into the system or downloaded by an operator, and performs up to eighth order linearization.
    Keywords: Acoustics
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  • 36
    Publication Date: 2019-07-10
    Description: A method for forming a sensor includes providing a first and a second film and bonding an internal connection tab there between. The internal connection tab is positioned between the inner surfaces of the first and second film. Then, a conductive adhesive is applied to either the tab or to the inner film surfaces such that the inner surfaces of the film and the tab are electrically connected. Finally, the films are pressed together to bond the film together with the internal connection tab in between.
    Keywords: Acoustics
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  • 37
    Publication Date: 2019-07-13
    Description: Researchers at NASA Langley Research Center have extensive experience using active structural acoustic control (ASAC) for aircraft interior noise reduction. One aspect of ASAC involves the selection of optimum locations for microphone sensors and force actuators. This paper explains the importance of sensor/actuator selection, reviews optimization techniques, and summarizes experimental and numerical results. Three combinatorial optimization problems are described. Two involve the determination of the number and position of piezoelectric actuators, and the other involves the determination of the number and location of the sensors. For each case, a solution method is suggested, and typical results are examined. The first case, a simplified problem with simulated data, is used to illustrate the method. The second and third cases are more representative of the potential of the method and use measured data. The three case studies and laboratory test results establish the usefulness of the numerical methods.
    Keywords: Acoustics
    Type: AIAA Paper 98-1865 , Structures, Structural Dynamics and Materials; Apr 20, 1998 - Apr 23, 1998; Long Beach, CA; United States
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  • 38
    Publication Date: 2019-07-13
    Description: The primary effort of this research project was focused the development of analytical methods for the accurate prediction of structural acoustic noise and response. Of particular interest was the development of curved frame and shell spectral elements for the efficient computational of structural response and of schemes to match this to the surrounding fluid.
    Keywords: Acoustics
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  • 39
    Publication Date: 2019-07-13
    Description: This report covers the third year research effort of the project. The research work focussed on the fine scale mixing noise of both subsonic and supersonic jets and the effects of nozzle geometry and tabs on subsonic jet noise. In publication 1, a new semi-empirical theory of jet mixing noise from fine scale turbulence is developed. By an analogy to gas kinetic theory, it is shown that the source of noise is related to the time fluctuations of the turbulence kinetic theory. On starting with the Reynolds Averaged Navier-Stokes equations, a formula for the radiated noise is derived. An empirical model of the space-time correlation function of the turbulence kinetic energy is adopted. The form of the model is in good agreement with the space-time two-point velocity correlation function measured by Davies and coworkers. The parameters of the correlation are related to the parameters of the k-epsilon turbulence model. Thus the theory is self-contained. Extensive comparisons between the computed noise spectrum of the theory and experimental measured have been carried out. The parameters include jet Mach number from 0.3 to 2.0 and temperature ratio from 1.0 to 4.8. Excellent agreements are found in the spectrum shape, noise intensity and directivity. It is envisaged that the theory would supercede all semi-empirical and totally empirical jet noise prediction methods in current use.
    Keywords: Acoustics
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  • 40
    Publication Date: 2019-07-13
    Description: The noise from perfectly expanded coaxial jets was measured in an anechoic chamber for different operating conditions with the same total thrust, mass flow, and exit area. The shape of the measured noise spectrum at different angles to the jet axis was found to agree with spectral shapes for single, axisymmetric jets. Based on these spectra, the sound was characterized as being generated by large turbulent structures or fine-scale turbulence. Modeling the large scale structures as instability waves, a stability analysis was conducted for the coaxial jets to identify the growing and decaying instability waves in each shear layer and predict their noise radiation pattern outside the jet. When compared to measured directivity, the analysis identified the region downstream of the outer potential core, where the two shear layers were merging, as the source of the peak radiated noise where instability waves, with their origin in the inner shear layer, reach their maximum amplitude. Numerical computations were also performed using a linearized Euler equation solver. Those results were compared to both the results from the instability wave analysis and to measured data.
    Keywords: Acoustics
    Type: NASA/TM-1998-207422 , E-11179 , NAS 1.15:207422 , AIAA Paper 98-2294 , Aeroacoustics; Jun 02, 1998 - Jun 04, 1998; Toulouse; France
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  • 41
    Publication Date: 2019-07-13
    Description: Airframe noise contributes the most to the environmental contamination from airports during take-off and landing. Two sources of noise are from the vortex-system associated with the slat and flap of multi-element wing designs. The flap-side edge vortex experiences bursting, known as vortex breakdown, at a critical deflection angle and experimental results show that this event may be one source of increased noise levels. Understanding of the edge roll-up phenomenon has increased but further focused studies on the role of the growth and bursting of the vortex structure are needed. The goal of the research is to plan a research program that will contribute to the understanding of the fluid physics of vortex breakdown and its relationship to noise production. The success of this program will lead to a priori predictions of when vortex breakdown will occur on the flap side-edge and accurate calculations of its effect on the noise level experienced by an observer near the aircraft during take-off and landing.
    Keywords: Acoustics
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  • 42
    Publication Date: 2019-07-13
    Description: There is renewed interest in the study of supersonic jets due to advances in high speed jet propulsion, supersonic combustion, and jet noise suppression for the next generation supersonic commercial transport. Understanding fundamental fluid dynamic and acoustic processes for these applications requires quantitative velocity, density and temperature measurements. In this paper we present data demonstrating a new, robust interferometer that can provide accurate data even in the presence of intense acoustic fields. This novel interferometer, the Liquid Crystal Point Diffraction Interferometer (LCPDI), was developed earlier for space flight experiments and is applied here to the case of a supersonic shock-containing jet. The LCPDI is briefly described, then integrated line-of-sight density data from the LCPDI for two underexpanded free jets are presented. The experimental shock spacings agree well with theory.
    Keywords: Acoustics
    Type: High Speed Jet Flows; Jun 21, 1998 - Jun 25, 1998; Washington, DC; United States
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  • 43
    Publication Date: 2019-07-13
    Description: Acoustic receptivity is the process by which acoustic disturbances are internalized into the shear layer to generate instability waves. Experiments have shown that, when tuned to the eigenvalue modes, the amplitude of the resulting T-S waves scales with the acoustic field intensity. When a surface irregularity is present, the characteristic wall wavenumber forces a spatial mode onto the near-wall mean velocity field, thus providing modal length scales comparable to those of T-S waves. In this experiment an attempt was made to increase the acoustic receptivity by exciting a difference mode via a quadratic interaction between two larger-wavenumber, forced modes. The difference mode is tuned to the dominant T-S eigenmode wavenumber. As expected, an increased receptivity corresponding to the difference mode was measured downstream of branch I, suggesting the presence of the nonlinearity.
    Keywords: Acoustics
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  • 44
    Publication Date: 2019-07-13
    Description: An imperfectly expanded supersonic jet, invariably, radiates both broadband noise and discrete frequency sound called screech tones. Screech tones are known to be generated by a feedback loop driven by the large scale instability waves of the jet flow. Inside the jet plume is a quasi-periodic shock cell structure. The interaction of the instability waves and the shock cell structure, as the former propagates through the latter, is responsible for the generation of the tones. Presently, there are formulas that can predict the tone frequency fairly accurately. However, there is no known way to predict the screech tone intensity. In this work, the screech phenomenon of an axisymmetric jet at low supersonic Mach number is reproduced by numerical simulation. The computed mean velocity profiles and the shock cell pressure distribution of the jet are found to be in good agreement with experimental measurements. The same is true with the simulated screech frequency. Calculated screech tone intensity and directivity at selected jet Mach number are reported in this paper. The present results demonstrate that numerical simulation using computational aeroacoustics methods offers not only a reliable way to determine the screech tone intensity and directivity but also an opportunity to study the physics and detailed mechanisms of the phenomenon by an entirely new approach.
    Keywords: Acoustics
    Type: NASA/CR-1998-207286 , NAS 1.26:207286 , AIAA Paper 98-0283 , Aerospace Sciences Meeting and Exhibit; Jan 12, 1998 - Jan 15, 1998; Reno, NV; United States
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  • 45
    Publication Date: 2019-07-10
    Description: The objective of this project is to investigate the possible use of adaptive digital filtering techniques in simultaneous, multiple-mode identification of the modal parameters of a vibrating structure in real-time. It is intended that the results obtained from this project will be used for state estimation needed in adaptive structural acoustics control. The work done in this project is basically an extension of the work on real-time single mode identification, which was performed successfully using a digital signal processor (DSP) at NASA, Langley. Initially, in this investigation the single mode identification work was duplicated on a different processor, namely the Texas Instruments TMS32OC40 DSP. The system identification results for the single mode case were very good. Then an algorithm for simultaneous two mode identification was developed and tested using analytical simulation. When it successfully performed the expected tasks, it was implemented in real-time on the DSP system to identify the first two modes of vibration of a cantilever aluminum beam. The results of the simultaneous two mode case were good but some problems were identified related to frequency warping and spurious mode identification. The frequency warping problem was found to be due to the bilinear transformation used in the algorithm to convert the system transfer function from the continuous-time domain to the discrete-time domain. An alternative approach was developed to rectify the problem. The spurious mode identification problem was found to be associated with high sampling rates. Noise in the signal is suspected to be the cause of this problem but further investigation will be needed to clarify the cause. For simultaneous identification of more than two modes, it was found that theoretically an adaptive digital filter can be designed to identify the required number of modes, but the algebra became very complex which made it impossible to implement in the DSP system used in this study. The on-line identification algorithm developed in this research will be useful in constructing a state estimator for feedback vibration control.
    Keywords: Acoustics
    Type: KU-FRL-1178-2
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  • 46
    facet.materialart.
    Unknown
    In:  CASI
    Publication Date: 2019-07-10
    Description: The National Aeronautics and Space Administration has established a goal of a 20 EPNdB reduction of aircraft noise by the year 2017. This paper proposes a fan concept for an engine that may meet this noise goal. The concept builds upon technology established during the Advanced Subsonic Technology Program which should show a 10 dB reduction potential. The new concept uses a two stage fan which allows low tip speed while still maintaining a reasonable total pressure rise across the two stages. The concept also incorporates many other noise reduction techniques in addition to low tip speed including a low number of exit guide vanes, swept and leaned guide vanes, a high subsonic Mach number inlet and syncrophased rotors to obtain active noise cancellation. The fan proposed in this paper is calculated to be able to achieve the 2017 noise goal.
    Keywords: Acoustics
    Type: NASA/TM-1998-208663 , NAS 1.15:208663 , E-11384
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  • 47
    Publication Date: 2019-07-10
    Description: This project deals with developing advanced methods for investigating and controlling interior noise in aircraft. The work concentrates on developing and applying the techniques of Near Field Acoustic Holography (NAH) and Principal Component Analysis (PCA) to the aircraft interior noise dynamic problem. This involves investigating the current state of the art, developing new techniques and then applying them to the particular problem being studied. The knowledge gained under the first part of the project was then used to develop and apply new, advanced noise control techniques for reducing interior noise. A new fully active control approach based on the PCA was developed and implemented on a test cylinder. Finally an active-passive approach based on tunable vibration absorbers was to be developed and analytically applied to a range of test structures from simple plates to aircraft fuselages.
    Keywords: Acoustics
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  • 48
    Publication Date: 2019-07-10
    Description: Blade-Vortex-Interaction (BVI) produces annoying high-intensity impulsive noise. NASA Ames collected several sets of BVI noise data during in-flight and wind tunnel tests. The goal of this work is to extract the essential features of the BVI signals from the in-flight data and examine the feasibility of extracting those features from BVI noise recorded inside a large wind tunnel. BVI noise generating mechanisms and BVI radiation patterns an are considered and a simple mathematical-physical model is presented. It allows the construction of simple synthetic BVI events that are comparable to free flight data. The boundary effects of the wind tunnel floor and ceiling are identified and more complex synthetic BVI events are constructed to account for features observed in the wind tunnel data. It is demonstrated that improved recording of BVI events can be attained by changing the geometry of the rotor hub, floor, ceiling and microphone. The Euclidean distance measure is used to align BVI events from each blade and improved BVI signals are obtained by time-domain averaging the aligned data. The differences between BVI events for individual blades are then apparent. Removal of wind tunnel background noise by optimal Wiener-filtering is shown to be effective provided representative noise-only data have been recorded. Elimination of wind tunnel reflections by cepstral and optimal filtering deconvolution is examined. It is seen that the cepstral method is not applicable but that a pragmatic optimal filtering approach gives encouraging results. Recommendations for further work include: altering measurement geometry, real-time data observation and evaluation, examining reflection signals (particularly those from the ceiling) and performing further analysis of expected BVI signals for flight conditions of interest so that microphone placement can be optimized for each condition.
    Keywords: Acoustics
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  • 49
    Publication Date: 2019-07-10
    Description: The non-equilibrium critical-layer analysis of a system of frequency-detuned resonant-triads is presented. In this part of the analysis, the system of partial differential critical-layer equations derived in Part I is solved analytically to yield the amplitude equations which are analyzed using a combination of asymptotic and numerical methods. Numerical solutions of the inviscid non-equilibrium oblique-mode amplitude equations show that the frequency-detuned self-interaction enhances the growth of the lower-frequency oblique modes more than the higher-frequency ones. All amplitudes become singular at the same finite downstream position. The frequency detuning delays the occurrence of the singularity. The spanwise-periodic mean-flow distortion and low-frequency nonlinear modes are generated by the critical-layer interaction between frequency-detuned oblique modes. The nonlinear mean flow and higher harmonics as well as the primary instabilities become as large as the base mean flow in the inviscid wall layer in the downstream region where the distance from the singularity is of the order of the wavelength scale.
    Keywords: Acoustics
    Type: NASA/CR-1998-208679 , NAS 1.26:208679 , E-11416
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  • 50
    facet.materialart.
    Unknown
    In:  CASI
    Publication Date: 2019-07-10
    Description: The National Aeronautics and Space Administration has established a goal of a 20 EPNdB reduction of aircraft noise by the year 2017. This paper proposes a fan concept for an engine that may meet this noise goal. The concept builds upon technology established during the Advanced Subsonic Technology Program which should show a 10 dB reduction potential. The new concept uses a two stage fan which allows low tip speed while still maintaining a reasonable total pressure rise across the two stages. The concept also incorporates many other noise reduction techniques in addition to low tip speed including a low number of exit guide vanes, swept and leaned guide vanes, a high subsonic Mach number inlet and syncrophased rotors to obtain active noise cancellation. The fan proposed in this paper is calculated to be able to achieve the 2017 noise goal.
    Keywords: Acoustics
    Type: NASA /TM-1998-208663 , E-11384 , NAS 1.15:208663
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  • 51
    Publication Date: 2019-07-12
    Description: Adaptive compressive gain and level dependent spectral shaping circuitry for a hearing aid include a microphone to produce an input signal and a plurality of channels connected to a common circuit output. Each channel has a preset frequency response. Each channel includes a filter with a preset frequency response to receive the input signal and to produce a filtered signal, a channel amplifier to amplify the filtered signal to produce a channel output signal, a threshold register to establish a channel threshold level, and a gain circuit. The gain circuit increases the gain of the channel amplifier when the channel output signal falls below the channel threshold level and decreases the gain of the channel amplifier when the channel output signal rises above the channel threshold level. A transducer produces sound in response to the signal passed by the common circuit output.
    Keywords: Acoustics
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  • 52
    Publication Date: 2019-07-12
    Description: Adaptive compressive gain and level dependent spectral shaping circuitry for a hearing aid include a microphone to produce an input signal and a plurality of channels connected to a common circuit output. Each channel has a preset frequency response. Each channel includes a filter with a preset frequency response to receive the input signal and to produce a filtered signal, a channel amplifier to amplify the filtered signal to produce a channel output signal, a threshold register to establish a channel threshold level, and a gain circuit. The gain circuit increases the gain of the channel amplifier when the channel output signal falls below the channel threshold level and decreases the gain of the channel amplifier when the channel output signal rises above the channel threshold level. A transducer produces sound in response to the signal passed by the common circuit output.
    Keywords: Acoustics
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  • 53
    Publication Date: 2019-07-10
    Description: The reduction of aircraft cabin sound levels to acceptable values still remains a topic of much research. The use of conventional passive approaches has been extensively studied and implemented. However performance limits of these techniques have been reached. In this project, new techniques for understanding the structural acoustic behavior of aircraft fuselages and the use of this knowledge in developing advanced new control approaches are investigated. A central feature of the project is the Aircraft Fuselage Test Facility at Va Tech which is based around a full scale Cessna Citation III fuselage. The work is divided into two main parts; the first part investigates the use of an inverse technique for identifying dominant fuselage vibrations. The second part studies the development and implementation of active and active-passive techniques for controlling aircraft interior noise.
    Keywords: Acoustics
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  • 54
    Publication Date: 2019-07-10
    Description: A mathematical model is developed to describe the sound emitted from an arbitrary point within a turbulent flow near solid boundaries. A unidirectional, transversely sheared mean flow is assumed, and the cross-section of the cold jet is of arbitrary shape. The analysis begins with Lilley's formulation of aerodynamic noise and, depending upon the specific model of turbulence used, leads via Fourier analysis to an expression for the spectral density of the intensity of the far-field sound emitted from a unit volume of turbulence. The expressions require solution of a reduced Green's function of Lilley's equation as well as certain moving axis velocity correlations of the turbulence. Integration over the entire flow field is required in order to predict the sound emitted by the complete flow. Calculations are presented for sound emitted from a plugflow jet exiting a semi-infinite flat duct. Polar plots of the far-field directivity show the dependence upon frequency and source position within the duct. Certain model problems are suggested to investigate the effect of duct termination, duct geometry, and mean flow shear upon the far-field sound.
    Keywords: Acoustics
    Type: NASA/TM-1998-207421 , NAS 1.15:207421 , E-11178
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  • 55
    Publication Date: 2019-07-10
    Description: Using MacCormack-type methods, a new class of highly accurate compact MacCormack-type schemes is derived which does not require a tridiagonal matrix inversion to obtain the spatial derivatives. Two examples are shown, and results of these schemes for three linear and nonlinear CAA Benchmark Problems are presented.
    Keywords: Acoustics
    Type: NASA/CR-1998-208672 , NAS 1.26:208672 , ICOMP-98-07 , E-11396
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  • 56
    Publication Date: 2019-07-10
    Description: The purposes of the subject test were to identify and quantify the mechanisms by which fan broadband noise is produced, and to assess the validity of such theoretical models of those mechanisms as may be available. The test was conducted with the Boeing 18-inch fan rig in the Boeing Low-Speed Aeroacoustic Facility (LSAF). The rig was designed to be particularly clean and geometrically simple to facilitate theoretical modeling and to minimize sources of interfering noise. The inlet is cylindrical and is equipped with a boundary layer suction system. The fan is typical of modern high-by-pass ratio designs but is capable of operating with or without fan exit guide vanes (stators), and there is only a single flow stream. Fan loading and tip clearance are adjustable. Instrumentation included measurements of fan performance, the unsteady flow field incident on the fan and stators, and far-field and in-duct acoustic fields. The acoustic results were manipulated to estimate the noise generated by different sources. Significant fan broadband noise was found to come from the rotor self-noise as measured with clean inflow and no boundary layer. The rotor tip clearance affected rotor self-noise somewhat. The interaction of the rotor with inlet boundary layer turbulence is also a significant source, and is strongly affected by rotor tip clearance. High level noise can be generated by a high-order nonuniform rotating at a fraction of the fan speed, at least when tip clearance and loading are both large. Stator-generated noise is the loudest of the significant sources, by a small margin, at least on this rig. Stator noise is significantly affected by propagation through the fan.
    Keywords: Acoustics
    Type: NASA/CR-1998-208704 , NAS 1.26:208704
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  • 57
    Publication Date: 2019-07-13
    Description: The accurate prediction of jet noise is possible only if the jet flow field can be predicted accurately. Predictions for the mean velocity and turbulence quantities in the jet flowfield are typically the product of a Reynolds-averaged Navier-Stokes solver coupled with a turbulence model. To evaluate the effectiveness of solvers and turbulence models in predicting those quantities most important to jet noise prediction, two CFD codes and several turbulence models were applied to a jet configuration over a range of jet temperatures for which experimental data is available.
    Keywords: Acoustics
    Type: AIAA Paper 98-0083 , Aeorspace Sciences; Jan 12, 1998 - Jan 15, 1998; Reno, NV; United States
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  • 58
    Publication Date: 2019-08-15
    Description: A method and apparatus for ultrasonic imaging which includes scanning a test specimen located in a test fixture in a predetermined scan pattern. Propagating and receiving reflected pulses of ultrasonic energy from an ultrasonic transducer directed to a surface of the test specimen. Detecting and generating data of both the amplitude and the depth of a defect in the test specimen from the pulses received from the test specimen. Merging the data of the amplitude and the data of the depth of the defect into composite data and then displaying the composite data in a three dimensional image whereby a mesh of both amplitude and depth data of the defect is displayed in a single image of the defect.
    Keywords: Acoustics
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  • 59
    Electronic Resource
    Electronic Resource
    Weinheim : Wiley-Blackwell
    Berichte der deutschen chemischen Gesellschaft 125 (1992), S. 9-14 
    ISSN: 0009-2940
    Keywords: Alkynyl groups ; Palladium, trimethylphosphane complexes ; Trimerization, oxidative ; Chemistry ; Inorganic Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology
    Notes: Oxidative Trimerization of Alkynyl Groups at Trimethylphosphane Palladium ComplexesAlkynylpalladium halides trans-PdX (C ≡ CR)(PMe3)2 [1, 2, 4, X = Cl, R = SiMe3, (CH2)2CH3, (CH2)5CH3; 3, X = Br, R = (CH2)2CH3] were synthesized by routine methods, while further examples of the series trans-PdX (C ≡ CR)(PMe3)2 [5, 7, 8, 10, X = Br, R = SiMe3, CMe3, (CH2)2CH3, Ph; 7, 9, 11, X = I, R = SiMe3, SiPh3, OEt] and trans-PdX (C ≡ CR)(PPh3)2 (12-14, X=I, R=SiMe3, CMe3, CH2OH) were obtained by oxidative addition of 1-halogeno-1-alkynes to PdL4 (L=PMe3, PPh3). Just above the melting point or decomposition point 5-7 are transformed by oxidative trimerization of the alkynyl groups to give enediynyl complexes trans-PdX[C(C ≡ CR)=C(C ≡ CR)R](PMe3)2 (15, 16, R=SiMe3, X=Br, I; 17, X=Br, R=CMe3). According to an X-ray structure analysis 17 has E configuration.
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    Berichte der deutschen chemischen Gesellschaft 125 (1992), S. 15-22 
    ISSN: 0009-2940
    Keywords: Boranes, trialkyl- ; Nitriles ; Condensation ; β-Diketimines ; Chemistry ; Inorganic Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology
    Notes: The reaction of trialkylboranes, e. g. triethylborane (Et3B), tripropylborane (Pr3B), or 9-alkyl-9-borabicyclo[3.3.1]nonane [alkyl-BBN; alkyl=Et, 1-methylpropyl, 1-methybutyl/1-ethylpropyl], with either aceto-, propio-, butyro-, pivalo-, and benzonitrile gives, depending on the reaction conditions used or the nitrile employed, either the substituted diazoniadibora-tetidines (1 a - c), products of partial hydroboration, or by condensation of two or three nitrile molecules, with or without a concomitant hydroboration, the C3BN2 heterocycles 2a - c, 8a/b, 9a - d, and 10a/b (X-ray structure analyses of 2a and 10b).
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    Berichte der deutschen chemischen Gesellschaft 125 (1992), S. 43-46 
    ISSN: 0009-2940
    Keywords: Helicobacter Pylori ; Bismuth ; (S)-Lactate ; Chemistry ; Inorganic Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology
    Notes: Metals in Biology and Medicine, III.  -  Bismuth Lactate: Synthesis and Structure of a Hydroxycarboxylate ComplexAs a compound of medical relevance, bismuth (S)-lactate was synthesized and structurally characterized (single-crystal X-ray diffraction). Exploiting the versatile coordination chemistry of carboxylate groups (chelating and bridging ligands), the crystal structure is based upon a three-dimensional network, showing bismuth in a high coordination number environment.
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    Berichte der deutschen chemischen Gesellschaft 125 (1992), S. 47-53 
    ISSN: 0009-2940
    Keywords: Silyl triflates ; Oligosilanes ; Chemistry ; Inorganic Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology
    Notes: Preparation of New Monomeric, Oligomeric, and Polymeric Silyl TriflatesThe highly reactive silyl triflates R3SiOSO2CF3 are valuable reagents in organosilicon chemistry. New triflate derivatives of mono- and oligosilanes have been prepared by substitution of phenyl groups or hydrogen atoms for the trifluoromethanesulfonyl group. The presence of the electron-withdrawing triflate group leads to a strong deactivation of the other substituents at the silicon atom, and the displacement of a second phenyl group at the same silicon atom is much slower than the first step. For this reason in the case of phenylated oligosilanes stepwise monosubstitution of the silicon atoms has been found. Other new oligomeric silyl triflates are obtained by reaction of silanediyl(triyl) bis(tris)(trifluoromethanesulfonates) with lithium derivatives of organosilicon compounds. Finally, the cleavage of silicon-phenyl bonds of poly[methyl(phenyl)silanes] by CF3SO3H leads to triflate derivatives of polysilanes.
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  • 63
    ISSN: 0009-2940
    Keywords: Lithium dicyanomethanide ; Sodium dicyanomethanide ; Dicyanomethanides, lithium, sodium, tetrabutylammonium salts ; Chemistry ; Inorganic Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology
    Notes: The Crystal Structures of {Li3(12-crown-4)2[HC(CN)2]3}, {Na(15-crown-5)[HC(CN)2]}, and {NaN(nBu)4[HC(CN)2]2 · THF}The preparation and the crystal structures of the title compounds 1 - 3 are described. 1 forms a polymeric chain structure, in which one of the lithium ions is linked by Li…NCC(H)CN… bridges. The remaining lithium ions form (12-crown-4)Li[NCC(H)CN] units, which are coordinated by one of the nitrogen atoms of the dicyanomethanide ions with the lithium ions of the chain. 2 forms an ion pair, in which the sodium ion is coordinated by the five oxygen atoms of the crown ether molecule and by one nitrogen atom of the dicyanomethanide ion. 3 has a threedimensional network, in which the sodium ions are coordinated in a distorted tetrahedral manner by the nitrogen atoms of the dicyanomethanide ions. In the cavities of the network the tetrabutylammonium ions and the THF molecules are found.
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    Berichte der deutschen chemischen Gesellschaft 125 (1992), S. 103-106 
    ISSN: 0009-2940
    Keywords: Alkynes ; Nickel complexes ; Stannenes ; Metallacycloalkenes ; Kinetic and thermodynamic reaction control ; Chemistry ; Inorganic Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology
    Notes: Synthesis, Structure, and Reactivity of a Stanna(II)-nickela(III)-cyclobutene KomplexesThe (ethyne)nickel(0) complex (iPr2PC2H4PiPr2)Ni(C2H2) (1) reacts with the stannene Sn[CH(SiMe3)2]2 below -30°C to yield the stanna(II)-nickela(II)-cyclobutene complex (iPr2PC2H4PiPr2)YYNiCH=YYCHSn[CH(SiMe3)2]2 (2; 83%) as the kinetically controlled product; 2 has been characterized by IR and NMR spectroscopy and an X-ray crystal-structure determination. The latter shows the central four-membered ring to be planar with a long Ni - Sn bond [2.626(1) Å]. According to the temperature-dependent NMR spectra, 2 dissociates reversibly in solution to the starting components. The synthesis reaction thus represents an equilibrium as long as the temperature is below 20°C. These observations indicate that the structural lability of the stanna(II)-nickela(II)-cyclobutene moiety is associated with the weakness of the Ni - Sn bond. The bonding situation in 2 is best described as an “inner complex” in which a stannyl anion is coordinated to a nickel(II) cation. An ethereal solution of 2 undergoes an oxidative addition of one ethyne C - H bond to the stannene at 20°C to give the Ni(0)/Sn(IV) complex iPr2PC2H4PiPr2)Ni({η2-HC≡CSn(H)[CH(SiMe3)2]2} (3) as the thermodynamically controlled product. Reaction of 3 with CO liberates the new alkyne ligand.
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    Berichte der deutschen chemischen Gesellschaft 125 (1992), S. 123-123 
    ISSN: 0009-2940
    Keywords: Chemistry ; Inorganic Chemistry
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    Berichte der deutschen chemischen Gesellschaft 125 (1992), S. 93-96 
    ISSN: 0009-2940
    Keywords: Diazaphosphiridine oxides ; Chemistry ; Inorganic Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology
    Notes: Synthesis, Structure, and Isomerization of Diazaphosphiridine OxidesHerrn Professor Joseph Grobe zum 60. Geburtstag gewidmet.The 1,2-Bis(alkyl)iminophosphane, Et3C  -  P=N  -  tBu (1), reacts with nitroso compounds, RNO (R=tBu, Ph), to form the diazaphosphiridine oxides, Et3C  -  YYP(=O)  -  NtBu  -  NYYR, 4a, b. While 4a (R=tBu) is thermally stable, 4b (R=Ph) isomerizes with formation of the benzodiazaphosphole oxide Et3C  -  YYP(= O)  -  NH  -  C6H4  -  NYYtBu (5). The corresponding phospholimine Et3C  -  YYP(=NtBu)  -  NH  -  C6H4  -  NYYtBu (7) has been obtained from 1 and azobenzene. The three-membered phosphorus heterocycle 4a has been characterized by X-ray structure analysis, which reveales some remarkable features.
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  • 67
    ISSN: 0009-2940
    Keywords: Zirconium porphyrins ; Hafnium porphyrins ; Porphyrin double-deckers ; Metal bisporphyrinates ; Chemistry ; Inorganic Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology
    Notes: The electrochemical oxidation of zirconium and hafnium double-deckers M(P)2 (M=Zr, Hf; P=OEP, TPP) (Scheme 1)2) leads to mono- and dications which show near infrared absorption bands which are of ≈ 2000 cm-1 higher energy than those of the corresponding cerium double-decker cations. [Zr(OEP)2]X, [Zr(OEP)2]X2, and [Zr(TPP)2]X (X=ClO4- and PF6-) are isolated after electrochemical oxidation and are characterized by IR and NMR spectroscopy. Magnetic susceptibility measurements (2 K 〈 T 〈 300 K) of the solids confirm the strong coupling of the electron spins in the diamagnetic dication salt [Zr(OEP)2][ClO4]2. The molecular structure of Zr(OEP)2 is elucidated by an X-ray structural analysis.
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  • 68
    ISSN: 0009-2940
    Keywords: Imido ligands ; Amido ligands ; Niobium complexes ; Tantalum complexes ; Chemistry ; Inorganic Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology
    Notes: Multiple Bonds between Main-Group Elements and Transition Metals, CII[1].  -  Volatile MN4 Metal Complexes of Niobium and Tantalum Containing Dimethylsilyl SubstituentsNiobium and tantalum complexes 4a and 4b of formula (Me2SiH)N=M[N(SiHMe2)2]3 (a: M=Nb; b: M=Ta) are formed from lithium bis(dimethylsilyl)amide and either MOCl3 (2a,b) or MCl5 (3a,b). No β-hydrogen decomposition of these compounds occurs under normal conditions.
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  • 69
    ISSN: 0009-2940
    Keywords: Carbonyl olefination ; μ-Methylene complexes ; Molybdenum complexes ; Chemistry ; Inorganic Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology
    Notes: Organomolybdenum and Organotungsten Reagents, II.  -  On the Carbonyl-Olefinating μ-Methylene Complex from Mo2Cl10 and Four Equivalents of MethyllithiumMo2Cl10 reacts at  -  70°C with 4 equivalents of methyllithium to give a methylated thermolabile molybdenum complex. At higher temperatures it forms a thermolabile carbonyl-olefinating reagent which according to NMR data is the μ-CH2 complex Cl3Mo(μ-CH2)2MoCl3 (2). Reactions of 2 with aldehydes, ketones, azomethines, and epoxides are described.
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    Berichte der deutschen chemischen Gesellschaft 125 (1992), S. 163-169 
    ISSN: 0009-2940
    Keywords: Iron ; organo reagents ; Chemistry ; Inorganic Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology
    Notes: Alkyliron and Alkylcobalt Reagents, III.  -  Nonstabilized Ironalkyls: Formation, Detection, and ChemoselectivityThe crystalline ate complex Me4FeLi2(Et2O)2 (1 d) described in the literature as well as the complexes MeFeCl (1a), Me2Fe (1b), Me3FeLi (1c), nBu2Fe (2 a), nBu4FeLi2 (2b), nOct2Fe (3a), nOct3FeLi (3b), and nOct4FeLi2 (3c) are prepared in situ by transmetallation of MeLi, nBuLi, and nOctLi with FeCl2 (readily available by in situ reduction of FeCl3 with MeLi). All these complexes have been subjected to reaction with organic substrates for the first time. Evidence for this transmetallation has been furnished by a novel test (referred to as “β-bromostyrene-ketone test”). In this test, involving addition of β-bromostyrene (4) and 4-methylpentan-2-one (5), the alkyllithium compounds alkylate selectively only the ketone and the alkyliron compounds almost exclusively the β-bromostyrene. The high preference of the alkyliron reagents for the alkylation of the β-bromostyryl residue has been utilized for regioselective butylations and octylations of 1-{4-[(Z)-2-bromoethenyl]phenyl}-ethanone (6). Moreover, in competition reactions with benzaldehyde/4-methylpentan-2-one the alkyliron reagents have been found to react usually specifically with aldehydes. The decomposition temperatures of the reagents 1a,b,c and 2b in THF have been determined to be 0, -10, 25, and -20°C, respectively.
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    Berichte der deutschen chemischen Gesellschaft 125 (1992), S. 243-246 
    ISSN: 0009-2940
    Keywords: Ene reaction ; Silanes, vinyl- ; Triazolinediones ; Cycloaddition ; Regioselectivity ; Diastereoselectivity ; Chemistry ; Inorganic Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology
    Notes: The ene reaction of 4-methyl-1,2,4-triazoline-3,5-dione (MTAD) with vinylsilanes 1 has been investigated. In all cases studied, only hydrogen abstraction geminal to the silyl group with formation of triazolidinediones 3 occurred, irrespective of the number and size of the substituents at the double bond. A mechanism with an aziridinium imide as intermediate is proposed to explain the observed regioselectivity and diastereoselectivity. For the former we invoke preferential cleavage of the C-N bond proximate to the silyl substituent on the aziridine ring, for the latter steric repulsion between the adjacent silyl and alkyl group controls the observed E-type stereochemistry. A new synthetic approach to the trisubstituted vinylsilane 1e based on reductive lithiation of the corresponding vinyl sulfide is described.
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    Berichte der deutschen chemischen Gesellschaft 125 (1992), S. 255-258 
    ISSN: 0009-2940
    Keywords: Cyclophane ; [3.3]Metacyclophane, conformation of ; Chemistry ; Inorganic Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology
    Notes: [3.3]Metacyclophanes with anti ConformationThe [3.3]metacyclophanes 5 and 9 with prevailing anti conformation were prepared by using different cyclisation techniques. 1H-NMR studies and X-ray structure analyses of both phanes 5 and 9 prove their unprecedented conformations.
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    Berichte der deutschen chemischen Gesellschaft 125 (1992), S. 119-121 
    ISSN: 0009-2940
    Keywords: Isocyanide ; Chromium complexes ; Chemistry ; Inorganic Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology
    Notes: The triisocyanide ligand CH3C(CH2NC)3 reacts with Cr-(CO)5(THF) depending on the stoichiometry to give the complexes CH3C(CH2NC)x[CH2NC - Cr(CO)5]3-x (x=1, 2). The complex CH3C(CH2NC)2[CH2NC  -  Cr(CO)5] has been characterized by an X-ray structure analysis allowing a direct comparison of the bonding parameters of coordinated and noncoordinated isocyanide ligands in the same molecule.
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    Berichte der deutschen chemischen Gesellschaft 125 (1992), S. 459-465 
    ISSN: 0009-2940
    Keywords: 1-Aza-4,6-adamantanedione derivatives synthesis ; Radical deoxygenation, nBu3SnH ; Ammonium salts ; Chemistry ; Inorganic Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology
    Notes: Synthesis and Deoxygenation of Substituted 1-Azaadamantane-4,6-diones1-Azaadamantanes 5 and a variety of derivatives are accessible by a triple Mannich reaction of 1,3-cyclohexanediones 1 with hexamethylenetetramine to yield the 1-azaadamantane-4,6-diones 2. Deoxygenation of the sterically hindered and non-enolizable β-dioxo group in 2 succeeds by radical processes. Treatment with NaBH4/MeOH and subsequent chlorination give the dichlorides 4, which are dehalogenated with nBu3SnH. Quaternary ammonium salts 6 are available in high yields.
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    Berichte der deutschen chemischen Gesellschaft 125 (1992), S. 479-484 
    ISSN: 0009-2940
    Keywords: Norcaranes, 7,7-dibromo- ; 1H-Cyclopropa[a]naphthalenes, 1,1-dibromo-1a,2,3,7b-tetrahydro- ; Carbene insertion ; Bicyclo[1.1.0]butane derivatives ; Bicyclo[3.2.0.02,7]heptane derivatives ; Chemistry ; Inorganic Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology
    Notes: Preparation of Phenyl-Substituted Derivatives of Tricyclo[4.1.0.02,7]heptane and 1,2,3,4-Tetrahydro-1,2,3-methenonaphthaleneThe phenyl derivatives 3, 4, and 13 of tricyclo[4.1.0.02,7]heptane (1) and 17, 20, and 22 of 1,2,3,4-tetrahydro-1,2,3-methenonaphthalene (2) have been prepared from the dibromocarbene adducts of 1-phenyl-1-cyclohexene, 3-phenyl-1-cyclohexene, 1,3-diphenyl-1-cyclohexene, 1,2-dihydro-2-phenylnaphthalene, 1,2-dihydro-4-phenylnaphthalene, and 1,2-dihydro-2,3-diphenylnaphthalene, respectively, by treatment with methyllithium. The dibromocarbene adduct 10 of 1,6-diphenyl-1-cyclohexene reacts with methyllithium to give the bicyclo[3.2.0.02,7]heptane 11.
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    Berichte der deutschen chemischen Gesellschaft 125 (1992), S. 515-524 
    ISSN: 0009-2940
    Keywords: Dimethylhydrazones, metalated ; Acylation, regioselective ; 1,3-Diketones ; α-Cyano dimethylhydrazones ; Chemistry ; Inorganic Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology
    Notes: Acyclic and cyclic unsymmetrical ketones 1 are regioselectively acylated via their corresponding metalated dimethyl-hydrazones 3 by using acid chlorides or anhydrides, arylnitriles, ethyl formate, carbon disulfide/methyl iodide, alkyl chloroformates, dialkyl carbonates, phenyl isocyanate, or phenyl isothiocyanate as acylating agents. Subsequent acidic hydrolysis leads to the 1,3-diketones 6 in acceptable to excellent overall yields. The tautomeric structure of the product hydrazones 4, 5, 7, and 8 is determined. Cyanation of 3 with cyanogen bromide affords the α-cyano dimethylhydrazones 9.
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    Berichte der deutschen chemischen Gesellschaft 125 (1992), S. 407-409 
    ISSN: 0009-2940
    Keywords: Arsenic pentafluoride - nitrile adducts ; Cyanogen compounds ; Hard-soft acid-base (HSAB) principle ; Chemistry ; Inorganic Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology
    Notes: The Coordination Behaviour of the Nitrogen Bases R - CN (R = H, Cl, I, CH3) and Pyridine towards AsF5 in SolutionThe coordination behaviour of the nitriles R - CN (R = H, Cl, I, CH3) and of pyridine towards the strong Lewis acid AsF5 in solution is investigated and discussed on the basis of the hardsoft acid-base (HSAB) principle. Solution equilibria are studied by means of 1H-NMR spectroscopy. For the equilibrium of HCN, ICN, and AsF5 with the corresponding coordinated Lewis acid - Lewis base adducts the estimated value for the equilibrium constant is in good agreement with the experimental data.
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    Berichte der deutschen chemischen Gesellschaft 125 (1992), S. 417-422 
    ISSN: 0009-2940
    Keywords: Selenocarboxylates, O-triorganosilyl ; Selenone esters ; Seleno-selenol rearrangement ; Chemistry ; Inorganic Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology
    Notes: A series of O-triorganosilyl selenocarboxylates 2 are prepared by the reaction of sodium or potassium selenocarboxylate 1 with triorganosilyl chlorides. The selenone esters 2 are stable towards heat, but labile towards moisture, and are formed via Se-triorganosilyl selenocarboxylate 3. In the mass spectrometer, isomerization of 2 to its less stable selenol ester 3 takes place, resembling the Schönberg thione-thiol rearrangement.
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    Berichte der deutschen chemischen Gesellschaft 125 (1992), S. 447-452 
    ISSN: 0009-2940
    Keywords: Chromoionophore ; Chromoacerand ; Cryptand ; Dipyrrin ; Metal complexes ; Chemistry ; Inorganic Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology
    Notes: A Dipyrrino Cryptand  -  Synthesis, Crystal Structure, Metal ComplexationThe orange red cryptand 1, containing a dipyrrin chromophore, has been synthesized in seven steps. Its C2-symmetrical X-ray structure exhibits a planar dipyrrin unit and a twisted but not collapsed crown ring, two of the ether oxygen atoms projecting outwards. The complexation of alkali and transition metal cations by this concave dyestuff leads to changes of the color and to strong shifts in the UV/Vis spectra.
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    Berichte der deutschen chemischen Gesellschaft 125 (1992), S. 453-458 
    ISSN: 0009-2940
    Keywords: 2,2′-Bipyridine ; Chiral ligand ; Palladium complexes ; Copper complexes ; Cobalt complexes ; Chemistry ; Inorganic Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology
    Notes: Optically active 2,2′-bipyridine (S,S)-1 was synthesized by radical cyclization and a nickel(0)-mediated coupling of enantiomerically pure bromopyridine (S)-8. Palladium, copper, and cobalt complexes of 1 were prepared. The solid-state structures of meso-1 and 11 were determined by X-ray crystal structure analysis.
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  • 81
    ISSN: 0009-2940
    Keywords: Silanes, acetyl-, Si-functional ; Silanol, acetyl-, crystal structure of ; Microbial reduction ; Chemistry ; Inorganic Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology
    Notes: Synthesis of the Si-Functional Acetylsilanes tBu(Me3SiCH2)[MeC(O)]SiF and tBu(Me3SiCH2)[MeC(O)]SiH as well as Synthesis and Crystal Structure of the Acetylsilanol tBu(Me3SiCH2)[MeC(O)]SiOH: Substrates for Microbial ReductionsThe racemic Si-functional acetylsilanes tBu(Me3SiCH2)[MeC(O)]SiF (1) and tBu(Me3SiCH2)[MeC(O)]SiH (2) and the racemic acetylsilanol tBu(Me3SiCH2)[MeC(O)]SiOH (3) were synthesized from Si(OMe)4 (4) as substrates for microbial reductions [4 → tBuSi(OMe)3 (5) → tBu(Me3SiCH2)Si(OMe)2 (6) → tBu(Me3SiCH2)SiF2 (7) → tBu(Me3SiCH2)[CH2 = C(OMe)]SiF (8) → 1; 8 → tBu(Me3SiCH2)[CH2 = C(OMe)]SiH (9) → 2; 6 → tBu(Me3SiCH2)[CH2 = C(OMe)]SiOMe (10) → 3]. Compounds 1-3 were found to be reduced by cells of Trigonopsis variabilis (DSM 70714) [≡ SiC(O)Me → ≡ SiCH(OH)Me]. The crystal and molecular structure of 3 was studied by singlecrystal X-ray diffraction. In the crystal, racemic 3 forms infinite chains built up by intermolecular O—H…O bonds between the hydroxyl and acetyl groups of molecules of the same absolute configuration.
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  • 82
    ISSN: 0009-2940
    Keywords: Bicyclo[1.1.0]butanes, rearrangement ; Tricyclo[4.1.0.02,7]heptanes, kinetics of thermolysis ; 1,2,3-Methenonaphthalenes, 1,2,3,4-tetrahydro-, kinetics of thermolysis ; Bicyclo[3.2.0]hept-6-ene derivatives ; Benzocycloheptene derivatives ; Chemistry ; Inorganic Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology
    Notes: On the Thermal Rearrangement of the Bicyclo[1.1.0]butane System. A Kinetic Investigation of the Conversion of Tricyclo[4.1.0.02,7]heptanes into Bicyclo[3.2.0]hept-6-enesTricyclo[4.1.0.02,7]heptane (7), its 1- (20) and 2-phenyl derivatives (22), tetracyclo[5.1.0.02,4.03,5]octane (17), 1,2,3,4-tetrahydro-1,2,3-methenonaphthalene (25) as well as its 1- (35), 2- (32), and 3-phenyl derivatives (27) have been thermolyzed in solution in the temperature range between 110 and 230° C. The activation parameters of these reactions have been determined. The parent hydrocarbon 7 is converted into bicyclo[3.2.0]hept-6-ene (11) in high yield, and the other substrates behave analogously, i.e. the cyclobutene derivatives 18, 21, 23, 26, 28, 33, 34, and 36 are formed. Arising from 27, the cyclobutene 28 is observed as intermediate, which is transformed rapidly to a mixture of the benzocycloheptenes 29 and 31. To undergo this ring enlargement, the other cyclobutenes require more severe conditions. The thermal rearrangements of 20, 22, and 27 are accompanied by parallel reactions, which have been identified as acid-catalized processes in the case of 22 and 27 giving rise to the norcarene derivatives 24 and 30, respectively. In 2-phenylmethenonanpthalene 32 two pathways to a cyclobutene derivative exist; they are found to be followed in a 82:18 ratio. The relative reaction rates of all substrates investigated can be interpreted in terms of a consistent mechanistic model. Accordingly, the tricyclo[4.1.0.02,7]heptane system is transformed in a concerted but highly asynchronous process to an (E,Z)-1,3-cycloheptadiene, which then undergoes a rapid conrotatory ring closure to yield the corresponding bicyclo[3.2.0]hept-6-ene.
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  • 83
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    Berichte der deutschen chemischen Gesellschaft 125 (1992), S. 679-689 
    ISSN: 0009-2940
    Keywords: 1,1′-Binaphthyls ; Diphosphanes ; Nickel complexes ; Palladium complexes ; Chemistry ; Inorganic Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology
    Notes: 16- and 18-membered diphospha macrocycles (8, 12, and 15) have been synthesized from the corresponding 1,1′-binaphthyl precursors (6, 11, and 14, resp.) and o-phenylenebis(phenylphosphane) by means of high-dilution conditions in 55, 49, and 87% yield. X-ray structure analyses of 8a, 8b, 12b, and 12b · NiCl2 reveal their distinctly different conformations and conformational changes caused by complexation. These structural features are reflected in the pronounced different tendency of the compounds concerned to form Ni(II) and Pd(II) complexes.
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  • 84
    ISSN: 0009-2940
    Keywords: Chalcogeno boron hydride ; Noradamantane structure ; Calculations, SCF ; Chemistry ; Inorganic Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology
    Notes: [(BH2)5S4]-: A New Chalcogeno Boron Hydride Anion with Noradamantane Structure - Theoretical Investigation of the Structure[1]The reaction of NaBH4/THF · BH3 with elemental sulfur produces Na[(BH2)5S4] (4a) with hydrogen evolution. These nucleophilic degradation reactions proceed via [H3B -μ2-S(B2H5)]- (1) and the intermediate 3 by loss of BH4- and cyclization. 4 can also be obtained by addition of 1 to 1,2,4,3,5-trithiadiborolane (5). 4 builds up a noradamantane-like skeleton B5S4. An X-ray structure determination of [(C6H5)4P] · 4 failed because of disordering of the anion. 1H-, 11B-NMR shifts and 1J(11B1H) coupling constants convey further structural information. Structural data have been calculated by SCF methods.
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  • 85
    ISSN: 0009-2940
    Keywords: Trichlorosilylation ; Chlorophosphanes ; Silylphosphanes ; Chemistry ; Inorganic Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology
    Notes: Reactions of Silicon-Silicon Bonds, 2[1]. - Trichlorosilylations of tert-Butyldichlorophosphane and tert-Butylbis(trimethylsilyl)phosphane with Hexachlorodisilane: Synthesis of New Bifunctional (Trichlorosilyl)phosphanesDi-tert-butyl(trimethylsilyl)phosphane (1) and tert-butylbis(trimethylsilyl)phosphane (3) react with one equivalent of hexachlorodisilane with exchange of one trimethylsilyl group by a trichlorosilyl group under mild conditions to give di-tert-butyl(trichlorosilyl)phosphane (2) and tert-butyl(trichlorosilyl)(trimethylsilyl)phosphane (4) in fair yields. tert-Butylbis(trichlorosilyl)phosphane (5) is available from tert-butyldichlorophosphane without organometallic reagents and solvents by simple reductive trichlorosilylation with the help of two equivalents of hexachlorodisilane. 5 is a useful precursor for phosphaalkane synthesis: with pivaloyl chloride, 5 leads to tert-butyl-[tert-butyl(trichlorosilyloxy)methylene]phosphane (6). From 4 with pivaloyl chloride mainly 6 and some known tert-butyl[tert-butyl(trimethylsilyloxy)methylene]phosphane (7) are formed.
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  • 86
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    Berichte der deutschen chemischen Gesellschaft 125 (1992), S. 675-677 
    ISSN: 0009-2940
    Keywords: 2,2′-Bisdimedonylidene, synthesis and electrophilic reactions of ; Olefin, electrophilic ; Chemistry ; Inorganic Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology
    Notes: „2,2′-Bisdimedonylidene‘ - a Novel Electrophilic OlefinHerrn Professor Michael Hanack zum 60. Geburtstag gewidmet.The title compound has been prepared unambiguously by dehydrogenation of known „2,2′-bisdimedonyl’ (8). Its typical electrophilic character leads to additions of various nucleophiles which prove the molecular structure. Physical data are in disagreement with those mentioned in the literature.
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  • 87
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    Berichte der deutschen chemischen Gesellschaft 125 (1992), S. 691-700 
    ISSN: 0009-2940
    Keywords: Cationic rearrangements ; Nitrenium ions ; Ion pairs ; Regio- and stereoselectivity ; NMR, 17O ; Chemistry ; Inorganic Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology
    Notes: Cationic Rearrangements of 2-Azabicyclo[3.2.0]heptane Systems. - NMR and MS Methods for the Analysis of 17O- or 18O-Labelled CompoundsO-Tosylation of 2-hydroxy-2-azabicyclo[3.2.0]hept-6-ene and -heptane results in rearrangements to 1-aza-[2.2.1] systems. The regioselectivity is caused by kinetic control. High stereose-lectivity, partial scrambling of the O-label and low yields in cross-over experiments agree with the intermediacy of tight ion pairs. - For the quantitative analysis of labelling, 17O-NMR, 13C-NMR and mass spectrometry are optimized and their efficiencies compared.
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  • 88
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    Berichte der deutschen chemischen Gesellschaft 125 (1992), S. 723-728 
    ISSN: 0009-2940
    Keywords: 1,8-Diaminonaphthalenes, X-ray structure analysis of, conformational barriers of, dynamic behavior of ; Chemistry ; Inorganic Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology
    Notes: The title compounds 2 and 3 have been synthesized from 1,8-diaminonaphthalene. The molecular structure of 2 has been determined by X-ray structure analysis and is discussed with regard to the arrangement of the peri-diphenylamino substituents in the crystalline state and the steric strain in the molecule. NMR studies of 3 reveal two conformational processes. Their nature is discussed and barriers are reported.
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  • 89
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    Berichte der deutschen chemischen Gesellschaft 125 (1992), S. 739-749 
    ISSN: 0009-2940
    Keywords: Cope rearrangement ; Diradicals ; Oxygen trapping ; Energy well ; Chemical activation ; Chemistry ; Inorganic Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology
    Notes: Nonconcerted Cope-Rearrangement? 1,2,6,7-Cyclodecatetraene ThermolysisFrom the pressure and oxygen dependence of the trapping rate a two-step mechanism for the Cope rearrangement of the title compound is deduced, its energy profile established, and the heat of formation of the intermediate diradical 3 determined. In contrast to the meso compound the rearrangement of the rac isomer proceeds by two competing processes, a concerted and a nonconcerted pathway. The different behavior of the meso and rac compound can be correlated to the boat and chair geometry of the respective transition states.
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  • 90
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    Berichte der deutschen chemischen Gesellschaft 125 (1992), S. 751-756 
    ISSN: 0009-2940
    Keywords: Transition-metal chemistry ; Hydrogen exchange ; Gas-phase oxidation ; Fourier-transform ion-cyclotrone resonance ; Tandem mass spectrometry ; Chemistry ; Inorganic Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology
    Notes: Gas-phase experiments on the Fe+-mediated oxidation of 2-propanol and ethanol by 1,3-butadiene are described. The reaction takes place at an atomic Fe+ centre, and labeling experiments uncover its specificity. While the gas-phase reaction of Fe(η4-C4H6)+ with 2-propanol occurs at collision-rate and the analysis of ligand-binding energies, in principle, favour a catalytic cycle for the Fe+-mediated dehydrogenation of 2-propanol by 1,3-butadiene, this conjecture is not born out experimentally due to complicating “side” processes. In addition to the specific interligand two-hydrogen-atom transfer from the alcohol to butadiene, the study of isotopomers reveals several hydrogen-exchange processes preceding dehydrogenation, dehydration, and alkene loss from (C4H6)Fe+ (alcohol) complexes.
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  • 91
    ISSN: 0009-2940
    Keywords: Phosphoranes, bis(methylene), isomerization of ; λ3-Phosphiranes ; Chemistry ; Inorganic Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology
    Notes: Bis(methylene)phosphoranes - Synthesis, Spectroscopic Investigations and Thermal Isomerizations to λ3-PhosphiranesA great number of differently substituted bis(methylene)phosphoranes 10 [R - P{ = C(SiMe3)2}2] are obtained by nucleophilic substitution from bis[bis(trimethylsilyl)methylene]-chlorophosphorane (8). The reactions of dichlorophosphanes 1 and methylenephosphanes 3 with lithium carbenoides 2 furnish the mixed derivatives 6 [R - P( = CR1R2)( = CR3R4)] and 7 [R - P( = C(SiMe3)2( = CR3R4)]. Among these the reaction of the sterically less hindered methylenephosphanes 3c, d [R2N - P = C(H)SiMe3, R = Et, iPr] with an excess of the lithium carbenoide 2b results in the formation of the σ4λ5-phosphiranes 11a, b {R2N - P[ = C(H)SiMe3]2}. The sterically highly demanding substituents in 10a - o render great thermal stability, while the mixed bis(methylene)phosphoranes 6, 7 rearrange to the corresponding σ4λ5-phosphiranes 15a-o. Investigations performed between 30 and 180°C reveal that all bis(methylene)phosphoranes, with the exception of 6c, k - m and 7e, can be isomerized. - The phosphino-substituted bis(methylene)phosphoranes 10k, 1 show different reactivity. Light-and thermally induced cleavage of the P - P bond, and dimerization of the corresponding fragments result in the formation of 14 and the diphosphanes 13a, b. The bis(methylene)phosphoranes 10a-o are investigated by UV and NMR spectroscopy.
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  • 92
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    Berichte der deutschen chemischen Gesellschaft 125 (1992), S. 793-800 
    ISSN: 0009-2940
    Keywords: o-Benzoquinone adducts ; Rearrangement reactions ; Elimination reactions ; 1,3,2-Diazaphospholidin-1-ium salts ; Chemistry ; Inorganic Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology
    Notes: o-Benzoquinone Adducts, Rearrangement and Elimination Reactions of 1,1,3-Trimethyl-1,3,2-diazaphospholidin-1-ium SaltsThe 1,1,3-Trimethyl-1,3,2-diazaphospholidin-1-ium Salts X- [1 (X = [Br, Y = NEt2), 2 (X = [BPh4], Y = Me), 3 (X = [BPh4], Y = Ph), 4 (X = [BPh4], Y = NEt2), 5 (X = [BPh4], Y = tBu)] were treated with o-benzoquinones. The reaction of 1 with tetrachloro-o-benzoquinone furnished the spirophosphorane 6 with an intact N → λ5P donor-acceptor interaction. The reaction of 2, 3, and 4 with 3,5-di-tert-butyl-o-benzoquinone furnished [BPh4]- [8 (Y = Me), 9 (Y = Ph), 10 (Y = NEt2)]. The reaction of 5 with 3,5-di-tert-butyl-o-benzoquinone yielded 7 which exhibited no significant N →λ5P donor-acceptor interaction. The rearrangement product 11 was formed in small amounts during the reaction of 5 with tetrachloro-o-benzoquinone; 11 was also prepared by an alternative route. Thermolysis of the 1,1,3-trimethyl-1,3,2-diazaphospholidin-1-ium salts X- [14 (X = Br), 15 (X = I)] in vacuo led, with elimination of methyl halide, to the 1,3,2-diazaphospholidines 16 (X = Br) and 17 (X = I). The salts were characterized by FAB-MS.
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  • 93
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    Berichte der deutschen chemischen Gesellschaft 125 (1992), S. 1079-1081 
    ISSN: 0009-2940
    Keywords: Iminoboranes ; Stannylenes ; Aminostannation ; Chemistry ; Inorganic Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology
    Notes: Addition of Stannylenes to IminoboranesIminoboranes tBuB ≡ NR (R = tBu, Mes: 1 a, b) undergo aminostannation by the diaminostannylene Sn[N(SiMe3)2]2 (2b) to give (Me3Si)2N-B(tBu) = NR-Sn-N(SiMe3)2 (4a, b). The stannylene 4 b remains monomeric in the crystal (space group P21/n). The cyclic diaminostannylene [-Sn-N(tBu)-SiMe2-N(tBu)-] (3 b), instead, simply adds the boranes 1 a, b across one of its Sn-N bonds to form the bicyclo[2.2.0]hexene-type products 5a, b.
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  • 94
    ISSN: 0009-2940
    Keywords: Bulky substituents ; Aluminum compounds ; Chemistry ; Inorganic Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology
    Notes: Synthesis and Structure of CpAlCl2 Compounds with Sterically Demanding Substituents (Cp = Me5C5, EtMe4C5)[1]The compounds Cp*AlCl2 (3) (Cp* = Me5C5) and Cp′AlCl2 (4) (Cp′ = EtMe4C5) have been prepared by the reaction of Cp*SiMe3 (1) and Cp′SiMe3 (2) with AlCl3. The single-crystal X-ray structures of 3 and 4 are reported.
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  • 95
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    Berichte der deutschen chemischen Gesellschaft 125 (1992), S. 1111-1118 
    ISSN: 0009-2940
    Keywords: Aldehyde reactions ; Ruthenium clusters ; Oxidative addition ; Chemistry ; Inorganic Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology
    Notes: Oxidative Addition of Aldehydes and Schiff Bases to Ru3(CO)12Aldehydes show a wide variation of their reactive behaviour towards Ru3(CO)12. Aliphatic and simple aromatic aldehydes form simple oxidative addition products Ru3(CO)10(μ-H)(μ-RC = O) (1) either not at all or in low yields as impure compounds, while under forcing conditions dinuclear ruthenium μ-carboxylate complexes or the hydride H2Ru4(CO)13 are formed. Electron-rich aldehydes give good yields of cluster type 1 (R = p-MeOC6H4, p-Me2NC6H4, ferrocenyl). Schiff bases behave similarly, their oxidative addition products being Ru3(CO)10(μ-H)(μ-RC = NR′) (10, R = C6H5, p-MeOC6H4, p-Me2NC6H4, R′ = C6H5, p-MeC6H4). Of the ortho-substituted benzaldehydes, the methoxy compound produces clusters 6 and 7 resulting from aldehyde oxidative addition and aromatic ortho metalation. Salicylaldehyde and its p-tolylimine give the compounds Ru3(CO)8(μ-η2-OC6H4CH = X)2 (9, 11, X = O, NC6H4Me) with a bridging phenolate and a terminally bound aldehydic O or Schiff base NR function. 3-Pyridinecarbaldehyde reacts quickly with Ru3(CO)12 to give products 8 derived from pyridine CH rather than aldehyde CH oxidative addition. The crystal structures of 9 and 11 were determined.
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  • 96
    ISSN: 0009-2940
    Keywords: Iron complexes, dinuclear ; μ-[Cyano(phosphano)alkylidene] ligands ; Chemistry ; Inorganic Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology
    Notes: Replacement of SMe2 at the pseudo-alkylidyne μ-carbon atom of [Fe2Cp2(CO)2(μ-CO){μ-C(CN)SMe2}]SO3CF3 by PR2H (PR2 = PEt2, PCyH, PPhH) results in the formation of the phosphonium salts [Fe2Cp2(CO)2(μ-CO){μ-C(CN)PHR2}]SO3CF3 which upon deprotonation with NEt3 yield the corresponding neutral complexes [Fe2Cp2(CO)2(μ-CO){μ-C(CN)PR2}]. These μ-(phosphanoalkylidene) complexes have been characterized on the basis of IR, 31P{1H}-, 1H-, and 13C{1H}-NMR spectra and by the X-ray molecular structure of [Fe2Cp2(CO)2(μ-CO){μ-C(CN)PEt2}].
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  • 97
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    Berichte der deutschen chemischen Gesellschaft 125 (1992), S. 1159-1167 
    ISSN: 0009-2940
    Keywords: Oligolactones, macrocyclic ; Macrocyclization ; Stannylene template ; Template synthesis ; Chemistry ; Inorganic Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology
    Notes: Dibutylstannylene-mediated macrolactonization of methyl 4,6-O-benzylidene-&7alpha;-D-glucopyranoside (2) with glutaryl and phthaloyl dichloride yields the respective dilactones 6e and 6f and parallel tetralactones 5e and 5f as well as the antiparallel tetralactone 4e in the case of glutarylation. The reaction with malonyl dichloride yields a negligible amount of the parallel tetralactone 5d and that of fumaryl and isophthaloyl dichloride yields polyesters only, a byproduct in all these reactions. The mechanism of stannylene-medidted macrolactonization is discussed incorporating data pertaining to known hexa- and octalactone formation when succinyl dichloride is used. A correlation between stannylene dimer symmetry and tetralactone constitutional isomer selectivity is introduced.
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  • 98
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    Berichte der deutschen chemischen Gesellschaft 125 (1992), S. 1191-1203 
    ISSN: 0009-2940
    Keywords: Asymmetric alkylation ; Pyridines, optically active ; Chiral ligands ; Asymmetric synthesis ; Enantioselective catalysis ; Chemistry ; Inorganic Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology
    Notes: Enantioselective alkylation of a variety of aldehydes with diethylzinc was achieved by using catalytic amounts of optically active pyridines and C2-symmetric 2,2′-bipyridines. The products were obtained in good yields with high enantioselectivities. Steric factors of the catalyst structure which govern the stereoselectivity were revealed, and important reaction intermediates were identified by spectroscopic means and singlecrystal X-ray diffraction. The effect of additives on the optical purity of the product was studied. A strong asymmetric amplification was found with catalysts of low ee′s.
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  • 99
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    Berichte der deutschen chemischen Gesellschaft 125 (1992), S. 1205-1215 
    ISSN: 0009-2940
    Keywords: Addition, conjugate ; Pyridines, optically active ; Chiral ligands ; Asymmetric synthesis ; Catalysis, enantioselective ; Chemistry ; Inorganic Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology
    Notes: Conjugate addition of diethylzinc to enones is catalyzed by a complex derived from Ni(acac)2 and C2-symmetric 2,2′-bipyridine 3 or chiral pyridines 5-12. The products are obtained with optical purities up to 89% ee. A strong positive nonlinear relationship between the enantiomeric excess of the ligand and the ee of the product has been observed. The factors which govern catalyst activity and enantioselectivity have been investigated.
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  • 100
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    Berichte der deutschen chemischen Gesellschaft 125 (1992), S. 1235-1241 
    ISSN: 0009-2940
    Keywords: Redox systems ; Electron transfer ; Hetero quinones ; Electron acceptors ; Thieno[3,2-b]thiophene derivatives ; Chemistry ; Inorganic Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology
    Notes: Multistep Reversible Redox Systems, LVIII[1]. - 2,5-Bis(cyanoimino)-2,5-dihydrothieno[3,2-b]thiophenes - a New Acceptor Type: Synthesis and Common PropertiesThe synthesis of a variety of substituted 2,5-bis(cyanoimino)-2,5-dihydrothieno[3,2-b]thiophenes (4) and the corresponding diones (5) is described. Different substituents on the acceptors 4 and 5 allow the redox potentials of these reversible two-step redox systems to be varied over a wide range.
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