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  • 1
    Electronic Resource
    Electronic Resource
    Chichester : Wiley-Blackwell
    Organic Magnetic Resonance 6 (1974), S. 195-199 
    ISSN: 0030-4921
    Keywords: Chemistry ; Analytical Chemistry and Spectroscopy
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology
    Description / Table of Contents: The qualitative and quantitative isotopic analysis of mixtures of nuclear isomers of ethanol C2H5-nDnOH is described. The samples are obtained by reduction reactions and in each of them an isomer is markedly predominant. After a mass spectrometric determination of the amount of isotopic species with the same overall deuteration, these species are identified by proton and deuteron NMR, by combining the spectral schemes of all the isomers which can be assumed until agreement is reached with experimental spectra; isotope effect on δ is taken into account. The importance of the isotopic varieties are then determined by integrating some characteristic lines, with variable accuacy. For each sample, the total intensities of methyl and methylene signals are also compared in proton and deuteron resonance. By elevating the temperature of the sample, one can see the fine structure of a methylene signal broadened by the deuteron quadrupole relaxation.
    Notes: On décrit l'analyse isotopique qualitative et quantitative de mélanges d'isomères nucléaires de l'éthanol C2H5-nDnOH, obtenus par diverses réactions de réduction et dans lesquels une des variétés domine nettement. Après détermination par spectrométrie de masse du pourcentage des variétés isotopiques de même deutériation globale, celles-ci sont identifiées par RMN protonique et deutonique en combinant les schémas spectraux de tous les isomères qui peuvent être envisagés jusqu'à concordance avec les spectres expérimentaux; on tient compte de l'effet isotopique sur δ. Les variétés isotopiques présentes sont ensuite dosées avec une précision variable par intégration de raies caractéristiques. On compare également pour chaque mélange les intensités globales des signaux méthyliques et méthyléniques en résonance du proton et du deuton. Pour les signaux méthyléniques, élargis par relaxation quadrupolaire du deuton, on fait apparaître les structures fines en augmentant la température de l'échantillon.
    Additional Material: 4 Ill.
    Type of Medium: Electronic Resource
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  • 2
    Publication Date: 2005-06-01
    Print ISSN: 1530-6984
    Electronic ISSN: 1530-6992
    Topics: Chemistry and Pharmacology , Physics
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  • 3
    Publication Date: 2013-03-16
    Description: Author(s): T. J. Huffman, Peng Xu, M. M. Qazilbash, E. J. Walter, H. Krakauer, Jiang Wei, D. H. Cobden, H. A. Bechtel, M. C. Martin, G. L. Carr, and D. N. Basov Vanadium dioxide (VO 2 ) undergoes a phase transition at a temperature of 340 K between an insulating monoclinic M 1 phase and a conducting rutile phase. Accurate measurements of possible anisotropy of the electronic properties and phonon features of VO 2 in the insulating monoclinic M 1 and metallic rut... [Phys. Rev. B 87, 115121] Published Fri Mar 15, 2013
    Keywords: Electronic structure and strongly correlated systems
    Print ISSN: 1098-0121
    Electronic ISSN: 1095-3795
    Topics: Physics
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  • 4
    Publication Date: 2013-06-18
    Description: Author(s): K. H. Miller, X. S. Xu, H. Berger, V. Craciun, Xiaoxiang Xi, C. Martin, G. L. Carr, and D. B. Tanner Reflection and transmission as a function of temperature (7–300 K and 5–300 K respectively) have been measured on single crystals of the multiferroic compound FeTe 2 O 5 Br utilizing light spanning from the far infrared to the visible. The complex dielectric function and other optical properties were ob... [Phys. Rev. B 87, 224108] Published Mon Jun 17, 2013
    Keywords: Structure, structural phase transitions, mechanical properties, defects
    Print ISSN: 1098-0121
    Electronic ISSN: 1095-3795
    Topics: Physics
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  • 5
    Publication Date: 1977-03-01
    Description: Techniques for reducing edge bias are discussed and a new approach, termed the linear expansion method, is presented. This method is applicable to a wide variety of plot shapes and sizes and is unbiased under very general assumptions about the forest tree spatial pattern. The accuracy and efficiency of the linear expansion method were compared with (i) no edge bias correction and (ii) corrections by plot image translation techniques for several forest stands and spatial patterns. Results indicated translation and the linear expansion method behaved equally well on square plots 0.08 ha in size. As the plot size diminished or its shape deviated from square, the linear expansion method provided greater accuracy and lower bias than translation techniques. The linear expansion method also provided useful accuracy on circular plots where translation was not feasible.
    Print ISSN: 0045-5067
    Electronic ISSN: 1208-6037
    Topics: Agriculture, Forestry, Horticulture, Fishery, Domestic Science, Nutrition
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  • 6
    Publication Date: 1978-06-01
    Description: Contour and three-dimensional representations were drawn by computer using data for Wisconsin. Utility of the technique and implications of the results are discussed.
    Print ISSN: 0045-5067
    Electronic ISSN: 1208-6037
    Topics: Agriculture, Forestry, Horticulture, Fishery, Domestic Science, Nutrition
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  • 7
    Publication Date: 2004-12-03
    Description: The M2.4-7A Arrow Wing HSCT configuration was optimized for straight and level cruise at a Mach number of 2.4 and a lift coefficient of 0.10. A quasi-Newton optimization scheme maximized the lift-to-drag ratio (by minimizing drag-to-lift) using Euler solutions from FL067 to estimate the lift and drag forces. A 1.675% wind-tunnel model of the Opt5 HSCT configuration was built to validate the design methodology. Experimental data gathered at the NASA Langley Unitary Plan Wind Tunnel (UPWT) section #2 facility verified CFL3D Euler and Navier-Stokes predictions of the Opt5 performance at the design point. In turn, CFL3D confirmed the improvement in the lift-to-drag ratio obtained during the optimization, thus validating the design procedure. A data base at off-design conditions was obtained during three wind-tunnel tests. The entry into NASA Langley UPWT section #2 obtained data at a free stream Mach number, M(sub infinity), of 2.55 as well as the design Mach number, M(sub infinity)=2.4. Data from a Mach number range of 1.8 to 2.4 was taken at UPWT section #1. Transonic and low supersonic Mach numbers, M(sub infinity)=0.6 to 1.2, was gathered at the NASA Langley 16 ft. Transonic Wind Tunnel (TWT). In addition to good agreement between CFD and experimental data, highlights from the wind-tunnel tests include a trip dot study suggesting a linear relationship between trip dot drag and Mach number, an aeroelastic study that measured the outboard wing deflection and twist, and a flap scheduling study that identifies the possibility of only one leading-edge and trailing-edge flap setting for transonic cruise and another for low supersonic acceleration.
    Keywords: Aircraft Design, Testing and Performance
    Type: First NASA/Industry High-Speed Research Configuration Aerodynamics Workshop; Part 3; 1041-1071; NASA/CP-1999-209690/PT3
    Format: text
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  • 8
    Publication Date: 2019-06-28
    Description: Published aircraft surface waviness and boundary layer transition measurements imply that currently achievable low levels of surface waviness are compatible with the natural laminar flow (NLF) requirements of business and commuter aircraft, in the cases of both metallic and composite material airframes. The primary challenge to the manufacture of NLF-compatible surfaces is two-dimensional roughness in the form of steps and gaps at structural joints. Attention is presently given to recent NASA investigations of manufacturing tolerance requirements for NLF surfaces, including flight experiment results.
    Keywords: AIRCRAFT DESIGN, TESTING AND PERFORMANCE
    Type: SAE PAPER 850863
    Format: text
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  • 9
    Publication Date: 2019-06-28
    Description: Improvements in performance and fuel efficiency are evaluated for five new configurations of a six place, single turboprop, business airplane derived from a conventional, aluminum construction baseline aircraft. Results show the greatest performance gains for enhancements in natural laminar flow. A conceptual diesel engine provides greater fuel efficiency but reduced performance. Less significant effects are produced by the utilization of composite materials construction or by reconfiguration from tractor to pusher propeller installation.
    Keywords: AIRCRAFT DESIGN, TESTING AND PERFORMANCE
    Type: NASA-CR-172361 , NAS 1.26:172361
    Format: application/pdf
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  • 10
    Publication Date: 2019-06-28
    Description: The advantages of replacing the conventional wing on a transatlantic business jet with a larger, strut braced wing of aspect ratio 25 were evaluated. The lifting struts reduce both the induced drag and structural weight of the heavier, high aspect ratio wing. Compared to the conventional airplane, the strut braced wing design offers significantly higher lift to drag ratios achieved at higher lift coefficients and, consequently, a combination of lower speeds and higher altitudes. The strut braced wing airplane provides fuel savings with an attendant increase in construction costs.
    Keywords: AERODYNAMICS
    Type: NASA-CR-159361
    Format: application/pdf
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