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  • 1
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    In:  Other Sources
    Publikationsdatum: 2011-08-24
    Beschreibung: We study the onset of a pure Marangoni convection in a liquid layer with two deformable interfaces in the no-gravity environment. Both oscillatory and stationary instabilities are considered for a wide range of parameters. It is shown that only stationary instability is possible when surface tension at the colder interface is lower than that at the hotter one. Oscillatory instability tends to disappear and to be replaced by the stationary instability with increase of the Prandtl number and decrease of surface tension at the colder interface.
    Schlagwort(e): FLUID MECHANICS AND HEAT TRANSFER
    Materialart: Advances in Space Research (ISSN 0273-1177); 16; 7; p. (7)83-(7)86
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  • 2
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    In:  Other Sources
    Publikationsdatum: 2011-08-24
    Beschreibung: A consistent solution of the radiative transfer equation characterizing photon transport in a semi-infinite medium of refractive index greater than or equal to one is obtained following the method of Sobolev. Fresnel specular reflection, Snell's law and isotropic scattering are assumed. An algorithm is developed and its accuracy is demonstrated. A numerical Laplace transform inversion leads to an efficient evaluation for the interior flux and source function distributions.
    Schlagwort(e): FLUID MECHANICS AND HEAT TRANSFER
    Materialart: Journal of Quantitative Spectroscopy & Radiative Transfer (ISSN 0022-4073); 53; 3; p. 257-267
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  • 3
    Publikationsdatum: 2011-08-24
    Beschreibung: Results are reported of the Surface Tension Driven Convection Experiment (STDCE) aboard USML-1 Spacelab. Steady and transient thermocapillary flows were investigated in a 10 cm dia. circular container filled with 10 Cs silicone oil. The velocity and temperature fields were studied in detail under various conditions. It is shown in this paper how the Marangoni number affects the velocity field. A numerical analysis of the flows was also conducted and its results were compared to the experimental data. Good agreement is shown.
    Schlagwort(e): FLUID MECHANICS AND HEAT TRANSFER
    Materialart: Advances in Space Research (ISSN 0273-1177); 16; 7; p. (7)79-(7)82
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  • 4
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    In:  CASI
    Publikationsdatum: 2004-10-30
    Schlagwort(e): FLUID MECHANICS AND HEAT TRANSFER
    Materialart: JPL Proc. of the Intern. Colloq. on Drop and Bubbles, Vol. 2; p 304-321
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  • 5
    Publikationsdatum: 2005-11-27
    Beschreibung: Fatigue crack length relationship with aircraft inspection intervals and structural reinforcement, high strength materials, and aircraft usage effects
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: NASA AIRCRAFT SAFETY AND OPERATING PROBL., VOL. 1 1971; P 391-401
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  • 6
    Publikationsdatum: 2005-11-27
    Beschreibung: Vibration design and test criteria considerations for space shuttle
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: NASA SPACE SHUTTLE TECHNOL. CONF., VOL. 3 APR. 1971; P 423-450
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  • 7
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    In:  CASI
    Publikationsdatum: 2005-11-27
    Beschreibung: Optimization of payload for space shuttle by reducing structural loading and weight
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: NASA SPACE SHUTTLE TECHNOL. CONF., VOL. 3 APR. 1971; P 315-332
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  • 8
    Publikationsdatum: 2005-11-27
    Beschreibung: Buffet response of straight wing and delta wing model of space shuttle launch configuration
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: NASA SPACE SHUTTLE TECHNOL. CONF., VOL. 3 APR. 1971; P 265-291
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  • 9
    Publikationsdatum: 2005-11-27
    Beschreibung: Transonic wind tunnel investigation of flow characteristics and pressure fluctuation of space shuttle launch and reentry configurations
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: NASA SPACE SHUTTLE TECHNOL. CONF., VOL. 3 APR. 1971; P 293-314
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  • 10
    Publikationsdatum: 2005-11-27
    Beschreibung: Parameters contributing to aeroelastic problems in thermal protection of space shuttle
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: NASA SPACE SHUTTLE TECHNOL. CONF., VOL. 3 APR. 1971; P 247-264
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  • 11
    Publikationsdatum: 2005-11-27
    Beschreibung: Application of research in panel flutter and boundary layer thickness to space shuttle
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: NASA SPACE SHUTTLE TECHNOL. CONF., VOL. 3 APR. 1971; P 231-245
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  • 12
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    In:  CASI
    Publikationsdatum: 2005-11-27
    Beschreibung: Transonic flutter and buffeting for elastic wind tunnel models of straight wing proposed for space shuttles
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: NASA SPACE SHUTTLE TECHNOL. CONF., VOL. 3 APR. 1971; P 201-229
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  • 13
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    In:  CASI
    Publikationsdatum: 2005-11-27
    Beschreibung: Problems in propellant dynamics including pipeline dynamics, effect of bubble location, turbulent flow, and effect of tilting tank on liquid oscillation frequency
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: NASA SPACE SHUTTLE TECHNOL. CONF., VOL. 3 APR. 1971; P 95-120
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  • 14
    Publikationsdatum: 2005-11-27
    Beschreibung: Dynamic response of thermal protection system panel for space shuttle
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: NASA. LANGLEY RES. CENTER NASA SPACE SHUTTLE TECHNOL. CONF., VOL. 3 APR. 1971; P 49-93
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  • 15
    Publikationsdatum: 2005-11-27
    Beschreibung: Vibration tests of space shuttle panels at room temperature
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: NASA SPACE SHUTTLE TECHNOL. CONF., VOL. 3 APR. 1971; P 27-48
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  • 16
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    In:  CASI
    Publikationsdatum: 2005-11-27
    Beschreibung: Vibration studies of dynamic scale model of space shuttle
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: NASA SPACE SHUTTLE TECHNOL. CONF., VOL. 3 APR. 1971; P 1-25
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  • 17
    Publikationsdatum: 2005-11-27
    Beschreibung: Theoretical calculations and holographic measurements on transverse deflections of astronomical mirror blank
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: NASA, WASHINGTON OPT. TELESCOPE TECHNOL. 1970; P 287-270
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  • 18
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    In:  CASI
    Publikationsdatum: 2005-11-27
    Beschreibung: Dynamic analysis to predict space vehicle response to atmospheric disturbances with reference to space shuttle
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: SPACE TRANSPORTATION SYSTEM TECHNOL. SYMP., VOL. 2 JUL. 1970; P 331-348
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  • 19
    Publikationsdatum: 2005-11-27
    Beschreibung: Load alleviation and structural mode control potential for space shuttle vehicle
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: SPACE TRANSPORTATION SYSTEM TECHNOL. SYMP., VOL. 2 JUL. 1970; P 349-363
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  • 20
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    In:  CASI
    Publikationsdatum: 2005-11-27
    Beschreibung: Basic vibration characteristics and random response in thin panels
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: SPACE TRANSPORTATION SYSTEM TECHNOL. SYMP., VOL. 2 JUL. 1970; P 43-57
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  • 21
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    In:  CASI
    Publikationsdatum: 2005-11-27
    Beschreibung: Communications satellite antenna structure dynamic response to random loads in launch environment
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: NASA. LEWIS RES. CENTER SPACE TRANSPORTATION SYSTEM TECHNOL. SYMP., VOL. 2 JUL. 1970; P 301-329
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  • 22
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    In:  CASI
    Publikationsdatum: 2005-11-27
    Beschreibung: Staging dynamics for piggyback space shuttles
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: NASA. LEWIS RES. CENTER SPACE TRANSPORTATION SYSTEM TECHNOL. SYMP., VOL. 2 JUL. 1970; P 123-142
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  • 23
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    In:  CASI
    Publikationsdatum: 2005-11-27
    Beschreibung: Lifting and control surface flutter on space shuttles
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: SPACE TRANSPORTATION SYSTEM TECHNOL. SYMP., VOL. 2 JUL. 1970; P 177-198
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  • 24
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    In:  CASI
    Publikationsdatum: 2005-11-27
    Beschreibung: Control systems for vibration isolation of large structures and vacuum chambers
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: NASA, WASHINGTON OPT. TELESCOPES TECHNOL. 1970; P 733-749
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  • 25
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    In:  CASI
    Publikationsdatum: 2005-11-27
    Beschreibung: Thermal environment effects on alignment behavior of structural joints and assemblies of reentry vehicle and Mars landing module
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: OPT. TELESCOPE TECHNOL. 1970; P 335-349
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  • 26
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    In:  CASI
    Publikationsdatum: 2005-11-27
    Beschreibung: Vibration response and acoustic fatigue characteristics of space shuttle thermal protection system design concepts
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: SPACE TRANSPORTATION SYSTEM TECHNOL. SYMP., VOL. 2 JUL. 1970; P 273-284
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  • 27
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    In:  CASI
    Publikationsdatum: 2005-11-27
    Beschreibung: Dynamic model for obtaining response data for space shuttle
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: SPACE TRANSPORTATION SYSTEM TECHNOL. SYMP., VOL. 2 JUL. 1970; P 29-42
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  • 28
    Publikationsdatum: 2005-11-27
    Beschreibung: Pogo effect influence on aerodynamic phenomena in rocket afterbody
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: NASA. LEWIS RES. CENTER SPACE TRANSPORTATION SYSTEM TECHNOL. SYMP., VOL. 2 JUL. 1970; P 263-265
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  • 29
    Publikationsdatum: 2005-11-30
    Beschreibung: The latest technology for structural analysis in relation to the design tasks that lie ahead for the space shuttle is reviewed. For shell-of-revolution structures, the analysis can be formulated as a one-dimensional problem which is readily solved by using finite-difference or numerical-integration techniques. For more general asymmetric shells, a two-dimensional formulation is required. However, the governing equations are readily formulated and are amenable to solution by finite-difference techniques. For a completely general structural arrangement, such as structural frameworks, recourse is usually made to discretized formulations using finite elements. Of course, the finite-element programs could be used for shell structures, but at a loss in accuracy and increase in computer time compared with the special purpose programs.
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: NASA Space Shuttle Technol. Conf.; p 685-725
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  • 30
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    In:  CASI
    Publikationsdatum: 2005-11-27
    Beschreibung: Ring reinforcements for damping structural deformation in orthotropic mirror design
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: NASA, WASHINGTON OPT. TELESCOPE TECHNOL. 1970; P 283-286
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  • 31
    Publikationsdatum: 2005-11-27
    Beschreibung: Finite element method for structural design of astronomical mirrors
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: NASA, WASHINGTON OPT. TELESCOPE TECHNOL. 1970; P 249-255
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  • 32
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    In:  CASI
    Publikationsdatum: 2005-11-27
    Beschreibung: Transient loading considerations for shuttle design
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: NASA. LEWIS RES. CENTER SPACE TRANSPORTATION SYSTEM TECHNOL. SYMP., VOL. 2 JUL. 1970; P 79-100
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  • 33
    Publikationsdatum: 2005-11-27
    Beschreibung: Assessment of techniques for determining eigenvalues of large systems
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: NASA. LEWIS RES. CENTER SPACE TRANSPORTATION SYSTEM TECHNOL. SYMP., VOL. 2 JUL. 1970; P 4-27
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  • 34
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    In:  CASI
    Publikationsdatum: 2005-11-27
    Beschreibung: Using finite element method in analysis and design of optical space telescopes
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: OPT. TELESCOPE TECHNOL. 1970; P 401-415
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  • 35
    Publikationsdatum: 2005-11-27
    Beschreibung: Structural analysis for optimal load carrying substrate members of lightweight astronomical mirror
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: NASA, WASHINGTON OPT. TELESCOPE TECHNOL. 1970; P 257-280
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  • 36
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    In:  CASI
    Publikationsdatum: 2005-11-27
    Beschreibung: User checklist for spacecraft boom selection with review of structural, electrical and mechanical properties
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: JPL PROC. OF THE 4TH AEROSPACE MECH. SYMP. 15 JAN. 1970; P 51-54
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  • 37
    Publikationsdatum: 2005-11-27
    Beschreibung: Acoustic, vibration, and shock environments in designing orbital telescopes
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: OPT. TELESCOPE TECHNOL. 1970; P 389-400
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  • 38
    Publikationsdatum: 2005-11-27
    Beschreibung: Coupled structure-propulsion system instability /POGO/ prevention on space shuttle
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: NASA. LEWIS RES. CENTER SPACE TRANSPORTATION SYSTEM TECHNOL. SYMP., VOL. 2 JUL. 1970; P 249-262
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  • 39
    Publikationsdatum: 2005-11-27
    Beschreibung: Supersonic panel flutter of space shuttle heat shields with flexible supports
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: SPACE TRANSPORTATION SYSTEM TECHNOL. SYMP., VOL. 2 JUL. 1970; P 199-221
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  • 40
    Publikationsdatum: 2005-11-27
    Beschreibung: Design and development of deployment fixture for simulated zero gravity testing of large area solar array
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: JPL PROC. OF THE 4TH AEROSPACE MECH. SYMP. 15 JAN. 1970; P 83-89
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  • 41
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    In:  CASI
    Publikationsdatum: 2005-11-27
    Beschreibung: Mechanical and thermal properties of materials for five spacecraft boom designs
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: JPL PROC. OF THE 4TH AEROSPACE MECH. SYMP. 15 JAN. 1970; P 43-45
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  • 42
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    In:  CASI
    Publikationsdatum: 2005-11-27
    Beschreibung: Customer opinion of design of aerospace mechanisms
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: JPL PROC. OF THE 4TH AEROSPACE MECH. SYMP. 15 JAN. 1970; P 91-94
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  • 43
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    In:  CASI
    Publikationsdatum: 2005-11-27
    Beschreibung: Performance summary and spacecraft applications of booms with future trends
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: JPL PROC. OF THE 4TH AEROSPACE MECH. SYMP. 15 JAN. 1970; P 55-72
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  • 44
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    In:  CASI
    Publikationsdatum: 2005-03-28
    Beschreibung: In many structures the final stress states are dependent on the sequence of construction or the stress states at various stages of construction are of interest. Such problems can be analyzed using finite element programs that have the capability of adding (birthing) elements to simulate the progress of construction. However, the usual procedure of assembling elements may lead to numerical instabilities or stress states that are unrealistic. Both problems are demonstrated in the analysis of a structure using the program ADINA. A technique which combines application of a preload with element birthing to overcome these problems is described and illustrated.
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: NASA. Langley Research Center Res. in Struct. and Dyn., 1984; p 395-404
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  • 45
    Publikationsdatum: 2005-03-28
    Beschreibung: A technique utilizing finite element analysis, liquid impact kinematics, and momentum theory is described and compared to single-drop impact test data performed on various configurations of coated ceramic material. The method correlates well with test data and is useful in predicting the single-drop impact damage velocity threshold for low-density, coated ceramic materials.
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: NASA. Langley Research Center Res. in Struct. and Dyn., 1984; p 385-393
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  • 46
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    In:  CASI
    Publikationsdatum: 2005-03-28
    Beschreibung: An algorithm is outlined for simulating the contact surface erosion for impact problems. The algorithm dynamically relocates the contact surface as projectile and target materials exceed their failure criterion. Example computations of axisymmetric and oblique impacts are compared with experimental data.
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: NASA. Langley Research Center Res. in Struct. and Dyn., 1984; p 315-324
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  • 47
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    In:  CASI
    Publikationsdatum: 2005-03-28
    Beschreibung: A study of the dynamic characteristics of a coupled translational-rotational system is given. The formulation of the problem considers the soil-structure interaction effects by utilizing the impedance functions at the foundation of a structure. Due to the fact that the coefficient matrix in the characteristic equation is frequency dependent in nature, iterations have to be performed to find the nature frequencies of the system. Examples and discussions are presented. Comparisons of the analytical results from various approaches are also given.
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: NASA. Langley Research Center Res. in Struct. and Dyn., 1984; p 289-296
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  • 48
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    In:  CASI
    Publikationsdatum: 2005-03-28
    Beschreibung: Two analytical techniques applicable to large deflection dynamic response calculations for pressure loaded composite sandwich panels are demonstrated. One technique utilizes finite element modeling with a single equivalent layer representing the face sheets and core. The other technique utilizes the modal analysis computer code DEPROP which was recently modified to include transverse shear deformation in a core layer. The example problem consists of a simply supported rectangular sandwich panel. Included are comparisons of linear and nonlinear static response calculations, in addition to dynamic response calculations.
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: NASA. Langley Research Center Res. in Struct. and Dyn., 1984; p 251-268
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  • 49
    Publikationsdatum: 2005-03-28
    Beschreibung: The design of thin shell structures with respect to elastoplastic buckling requires an extended analysis of the influence of initial imperfections. For conservative design, the most critical defect should be assumed with the maximum allowable magnitude. This defect is closely related to the initial postbuckling behavior. An algorithm is given for the quasi-static analysis of the postbuckling behavior of structures that exhibit multiple buckling points. the algorithm based upon an energy criterion allows the computation of the critical perturbation which will be employed for the definition of the critical defect. For computational efficiency, the algorithm uses the reduced basis technique with automatic update of the modal basis. The method is applied to the axisymmetric buckling of cylindrical shells under axial compression, and conclusions are given for future research.
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: NASA. Langley Research Center Res. in Struct. and Dyn., 1984; p 237-250
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  • 50
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    In:  CASI
    Publikationsdatum: 2005-03-28
    Beschreibung: A general approach is required for describing matter of behavior when the failure is likely to involve growth and coalescence of a large number of fractures. Failures of this kind appear frequently in rapid dynamic processes, particularly in the formation of spall fragments. An approach to formulating constitutive relations that accounts for the opening, shear and growth of an ensemble of cracks is discussed. The approach accounts for plastic flow accompanying fragmentation. The resulting constitutive relations were incorporated into a Lagrangian computer program. A theoretical approach to coalescence is described. The simplest formulation uses a linear Liouville equation, with crack growth limited by the mean free path of cracks, assumed constant. This approach allows for an anisotropic distribution of cracks. An alternative approach in which the decrease of the mean free path with increasing crack size is accounted for, but the crack distribution is assumed isotropic is described. A reduction of the governing Liouville equation to an ordinary differential equation of third order is possible, and the result can be used to determine how mean free path decreases with increasing crack size.
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: NASA. Langley Research Center Res. in Struct. and Dyn., 1984; p 185-195
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  • 51
    Publikationsdatum: 2005-03-28
    Beschreibung: The design of a composite panel requires some way of finding the minimum thickness laminate which will withstand the load requirements without failure. The mathematical complexity of this problem dictates the use of nonlinear optimization techniques. Specialized laminate optimization programs were developed which are compact and efficient enough to run on microcomputers. Only stresses at a point and inplane loads and deflections are considered. The programs are simple to use and require no knowledge of optimization. Techniques are developed which find minimum thickness laminates with either ply ratios or ply angles as design variables. A method is presented for finding the optimum orientation for the axis of symmetry of an orthotropic laminate. The orthotropic laminate program uses an approximate failure theory, which speed up computations dramatically.
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: NASA. Langley Research Center Res. in Struct. and Dyn., 1984; p 181-183
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  • 52
    Publikationsdatum: 2005-03-28
    Beschreibung: The evaluation of the total probability of a plastic collapse failure P sub f for a highly redundant structure of random interdependent plastic moments acted on by random interdepedent loads is a difficult and computationally very costly process. The evaluation of reasonable bounds to this probability requires the use of second moment algebra which involves man statistical parameters. A computer program which selects the best strategy for minimizing the interval between upper and lower bounds of P sub f is now in its final stage of development. The relative importance of various uncertainties involved in the computational process on the resulting bounds of P sub f, sensitivity is analyzed. Response sensitivities for both mode and system reliability of an ideal plastic portal frame are shown.
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: NASA. Langley Research Center Res. in Struct. and Dyn., 1984; p 159-179
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  • 53
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    In:  CASI
    Publikationsdatum: 2005-03-28
    Beschreibung: A finite element modeling technique which utilizes a triangular element called TSHEL with 45 degrees of freedom and seven point integration was tested for analysis of thin plate and shell structures. The element formulation is based on the degenerate solid shell concept and the mixed formulation with assumed independent inplane and transverse shear strains. The effectiveness of the present modeling technique which features combined use of elements with kinematic modes and those without kinematic modes to eliminate both locking and spurious kinematic modes at the global structural levels are shown.
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: NASA. Langley Research Center Res. in Struct. and Dyn., 1984; p 123-142
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  • 54
    Publikationsdatum: 2005-03-28
    Beschreibung: The stress derivative technique for control of keystoning deformation in under-integrated finte elements is based on expansion of the stress in a Taylor series about the element center and retention of additional terms beyond the constant stress term. It has the advantage over other control techniques that keystoning resistance is provided by actual rather than artificial material properties. Application of this technique to the quadrilateral ring elements used for modelling solids of revolution subjected to axisymmetric loads is described. In a cylindrical coordinate system additional terms appear in the formulation which must be dealt with in arriving at a workable keystoning control scheme.
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: NASA. Langley Research Center Res. in Struct. and Dyn., 1984; p 111-122
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  • 55
    Publikationsdatum: 2005-03-28
    Beschreibung: An existing program is currently being adapted to perform finite element analysis by distributing substructures over a network of four Apple IIe microcomputers connected to a shared disk. In this network, one microcomputer controls the entire process while the others perform the analysis on each substructure in parallel. This substructure analysis is used in an iterative, fully stressed, structural resizing procedure. This procedure allows experimentatation with resizing in which all analyses are not completed during a single iteration. This research gives some insight on how to configure multidiscriplinary analysis and optimization procedures for decomposable engineering systems using either high performance engineering workstations or a parallel processor supercomputer. In addition, the operational experience gained facilitates the implementation of analysis programs on these new computers when they become available in an engineering environment.
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: Res. in Struct. and Dyn., 1984; p 45-54
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  • 56
    Publikationsdatum: 2005-03-28
    Beschreibung: Described are the experiences gained from solving for the dynamic response of two simple structures on an experimental Multiple Instruction Multiple Data (MIMD) computer called the finite element machine. Introduced are MIMD computing concepts, describing how the concurrent algorithmic techniques implemented and giving results for the two example problems. The results show computational speedups of up to 7.83 using eight of the finite element machine processors and indicate that significant computational speedups are possible for large order structural computations.
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: Res. in Struct. and Dyn., 1984; p 31-44
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  • 57
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    In:  CASI
    Publikationsdatum: 2005-03-28
    Beschreibung: The FLEX/32 Multicomputer is a generic environment for cooperating multiple processors. The FLEX/32 supports a number of different processors, making it heterogeneous in terms of the instruction sets it supports, and homogeneous in its ability to provide consistent storage and input/output facilities to its differing processors. These facilities are accessed through standard 32-bit VMEbus connections. The FLEX/32 supports the full UNIX System V Operating System and languages associated with it, plus the extended ConCurrent C and Concurrent FORTRAN 77 languages that allow programming of concurrent software at a high level. Direct programming support at all levels is provided by the environment hardware for concurrent software execution and optimization, including hardware support for shared resource access arbitration, conditional critical region arbitration, and interprocessor messages.
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: NASA. Langley Research Center Res. in Struct. and Dyn., 1984; p 1-14
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  • 58
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    In:  CASI
    Publikationsdatum: 2005-03-28
    Beschreibung: Research aimed at faster, more cost effective parallel machines and algorithms for improving designer productivity with finite element computations is discussed. A set of 8 boards, containing 4 nearest neighbor connected arrays of commercially available floating point chips and substantial memory, are inserted into a commercially available machine. One-tenth Mflop (64 bit operation) processors provide an 89% efficiency when solving the equations arising in a finite element problem for a single variable regular grid of size 40 by 40 by 40. This is approximately 15 to 20 times faster than a much more expensive machine such as a VAX 11/780 used in double precision. The efficiency falls off as faster or more processors are envisaged because communication times become dominant. A novel successive overrelaxation algorithm which uses cyclic reduction in order to permit data transfer and computation to overlap in time is proposed.
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: NASA. Langley Research Center Res. in Struct. and Dyn., 1984; p 15-29
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  • 59
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    In:  CASI
    Publikationsdatum: 2004-10-30
    Schlagwort(e): FLUID MECHANICS AND HEAT TRANSFER
    Materialart: JPL Proc. of the Intern. Colloq. on Drops and Bubbles, Vol. 2; p 405-413
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  • 60
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    In:  CASI
    Publikationsdatum: 2004-10-30
    Schlagwort(e): FLUID MECHANICS AND HEAT TRANSFER
    Materialart: JPL Proc. of the Intern. Colloq. on Drops and Bubbles, Vol. 2; p 390-464
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  • 61
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    In:  CASI
    Publikationsdatum: 2004-10-30
    Schlagwort(e): FLUID MECHANICS AND HEAT TRANSFER
    Materialart: JPL Proc. of the Intern. Colloq. on Drops and Bubbles, Vol. 2; p 629-631
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  • 62
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    In:  CASI
    Publikationsdatum: 2004-10-30
    Schlagwort(e): FLUID MECHANICS AND HEAT TRANSFER
    Materialart: JPL Proc. of the Intern. Colloq. on Drops and Bubbles, Vol. 2; p 372-389
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  • 63
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    In:  CASI
    Publikationsdatum: 2004-10-30
    Schlagwort(e): FLUID MECHANICS AND HEAT TRANSFER
    Materialart: JPL Proc. of the Intern. Colloq. on Drops and Bubbles, Vol. 2; p 322-337
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  • 64
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    In:  CASI
    Publikationsdatum: 2004-10-30
    Schlagwort(e): FLUID MECHANICS AND HEAT TRANSFER
    Materialart: JPL Proc. of the Intern. Colloq. on Drops and Bubbles, Vol. 2; p 300-303
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  • 65
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    In:  CASI
    Publikationsdatum: 2004-10-30
    Schlagwort(e): FLUID MECHANICS AND HEAT TRANSFER
    Materialart: JPL Proc. of the Intern. Colloq. on Drops and Bubbles, Vol. 2; p 338-356
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  • 66
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    In:  CASI
    Publikationsdatum: 2004-10-30
    Beschreibung: Space shuttle liftoff dynamics
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: SPACE TRANSPORTATION SYSTEM TECNOL. SYMP., VOL. 2 JUL. 1970; P 101-122
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  • 67
    Publikationsdatum: 2004-10-30
    Schlagwort(e): FLUID MECHANICS AND HEAT TRANSFER
    Materialart: JPL Proc. of the Intern. Colloq. on Drops and Bubbles, Vol. 2; p 606-616
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  • 68
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    In:  CASI
    Publikationsdatum: 2004-10-30
    Schlagwort(e): FLUID MECHANICS AND HEAT TRANSFER
    Materialart: JPL Proc. of the Intern. Colloq. on Drops and Bubbles, Vol. 2; p 553-570
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  • 69
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    In:  CASI
    Publikationsdatum: 2004-10-30
    Schlagwort(e): FLUID MECHANICS AND HEAT TRANSFER
    Materialart: JPL Proc. of the Intern. Colloq. on Drops and Bubbles, Vol. 2; p 487-505
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  • 70
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    In:  CASI
    Publikationsdatum: 2004-10-30
    Schlagwort(e): FLUID MECHANICS AND HEAT TRANSFER
    Materialart: JPL Proc. of the Intern. Colloq. on Drops and Bubbles, Vol. 2; p 414-426
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  • 71
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    In:  CASI
    Publikationsdatum: 2004-10-30
    Schlagwort(e): FLUID MECHANICS AND HEAT TRANSFER
    Materialart: JPL Proc. of the Intern. Colloq. on Drops and Bubbles, Vol. 2; p 357-371
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  • 72
    Publikationsdatum: 2006-03-28
    Beschreibung: Cybernetics diagnostics of machines and mechanisms using the spectral approach is discussed. The problem of establishing the accuracy of determination of the spectral composition is investigated. In systems with rectilinear or rotary movement, the vibrations appear in the form of movement rate vibrations, which are equivalent to frequency modulation of the signal, in proportion to the mean movement rate of the body. The case of a harmonic signal which reproduces and analyzes the characteristics of the frequency modulated signal is discussed. Mathematical models are developed to show the relationships of the parameters.
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: Cybernetic Diagnostics of Mech. Systems with Vibro-acoustic Phenomena (NASA-TT-F-14899); p 275-278
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  • 73
    Publikationsdatum: 2006-03-28
    Beschreibung: Free vibrations of a system and vibrations which are multiples of them in frequency are discussed. The corresponding periodic forced vibrations of the type n/m (n is the number of periods of disturbance between periods of movement and m is the number of periods of movement in one period of disturbance), generated by a harmonic or close to harmonic disturbance, are propagated close to the corresponding curves of the free vibrations and their frequency multiples. It has been proposed that investigation of transitional modes of motion and capture regions be carried out by precise methods in phase space, with the least number of coordinates. Thus, for example, for nonautonomous second order equations (for example, the Duffing equations), in place of three variables (coordinates, velocity, phases), it is proposed to use two: velocity during transition of the coordinate through zero and phase.
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: Cybernetic Diagnostics of Mech. Systems with Vibro-acoustic Phenomena (NASA-TT-F-14899); p 256-259
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  • 74
    Publikationsdatum: 2006-03-28
    Beschreibung: A numerical analysis of the transitional modes of motion for a vibroshock system was conducted. The capture regions of the system are emphasized. The three initial parameters for a nonautonomous vibroshock system with one degree of freedom are identified as: (1) coordinates, (2) velocity, and (3) time. Mathematical models are developed to show the relationship of the parameters. Graphs are included to show the nature of the capture regions and to portray the trajectory of motion of mass with time, by solution of differential equations during increase and decrease in time.
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: Cybernetic Diagnostics of Mech. Systems with Vibro-acoustic Phenomena (NASA-TT-F-14899); p 250-255
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  • 75
    Publikationsdatum: 2006-03-28
    Beschreibung: A solution is given to the problem of a transient vibration process in a fastened plate, during a sudden displacement of the edge. Some partial cases of excitation are examined in which the packing can be calculated and the explicit type of change in a deformation over time can be found. Some examples are presented.
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: Cybernetic Diagnostics of Mech. Systems with Vibro-acoustic Phenomena (NASA-TT-F-14899); p 204-207
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  • 76
    Publikationsdatum: 2006-03-28
    Beschreibung: The method of automatic identification of acoustical signals, by means of the segmentation was used to investigate noises and vibrations in machines and mechanisms, for cybernetic diagnostics. The structural analysis consists of presentation of a noise or vibroacoustical signal as a sequence of segments, determined by the time quantization, in which each segment is characterized by specific spectral characteristics. The structural spectrum is plotted as a histogram of the segments, also as a relation of the probability density of appearance of a segment to the segment type. It is assumed that the conditions of ergodic processes are maintained.
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: Cybernetic Diagnostics of Mech. Systems with Vibro-acoustic Phenomena (NASA-TT-F-14899); p 179-180
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  • 77
    Publikationsdatum: 2006-03-28
    Beschreibung: An experimental investigation for estimating the nonlinearity of a diagnostic object was carried out on a single-stage, spur gear reducer. The linearity of the properties of spur gearing (including the linearity of its mode of operation) was tested. Torsional vibrations of the driven wheel and transverse (to the meshing plane) vibrations of the drive wheel on its support were taken as the two outputs of the object to be analyzed. The results of the investigation showed that the degree of nonlinearity of a reducing gear is essentially connected with its operating mode, so that different mathematical models of it can correspond to different values of the system parameters.
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: Cybernetic Diagnostics of Mech. Systems with Vibro-acoustic Phenomena (NASA-TT-F-14899); p 157-159
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  • 78
    Publikationsdatum: 2006-03-01
    Beschreibung: The stability of equilibrium shapes of elastic systems is examined. Stability loss in the case of similar equilibrium shapes, the disappearance of stable equilibrium shapes, and the disappearance of any forms of equilibrium are discussed. The error made by Euler in analyzing stability loss is pointed out, and Mises' truss is used as an example of stability loss in the case of similar equilibrium shapes.
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: Stability and Oscillation of Elastic Systems: Mod. Concepts, Paradoxes and Errors (NASA-TT-F-751); p 1-183
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  • 79
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    Publikationsdatum: 2006-03-01
    Beschreibung: Problems of oscillations of linear systems are discussed, including systems with a fractional number of degrees of freedom as well as free oscillations of a cantilever in the field of centrifugal forces. Four methods of solving the problem of the action of periodic instantaneous impulses are presented. The Tacoma catastrophe is analyzed and used as an example of aeroelastic oscillations. Problems of nonlinear system oscillations include the vibration maintenance of rotation, the Sommerfeld effect, and self-oscillations of a quasi-system with dry friction.
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: Stability and Oscillation of Elastic Systems: Mod. Concepts, Paradoxes and Errors NASA-TT-F-751); p 184-418
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  • 80
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    In:  CASI
    Publikationsdatum: 2006-02-14
    Beschreibung: The design, manufacture, and testing of an isolation system placed under a bench which simulates a space platform during testing in a hard vacuum are described. A low natural frequency isolation system is used to decouple ground vibrations from the bench. The materials used are vacuum compatible and do not introduce unwanted matter which would contaminate the payload optics and/or the testing environment. The system accommodates payloads of varying weights and envelopes.
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: NASA. Goddard Space Flight Center 13th Space Simulation Conf.; p 320-339
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  • 81
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    In:  CASI
    Publikationsdatum: 2006-02-14
    Beschreibung: The potential cost and performance advantages of welding was understood but ignored by solar panel manufacturers in the U.S. Although NASA, DOD and COMSAT have supported welding development efforts, soldering remains the only U.S. space qualified method for interconnecting solar cells. The reason is that no U.S. satellite prime contractor found it necessary, due to mission requirements, to abandon the space proven soldering process. It appears that the proposed NASA space station program will provide an array requirement, a 10 year operation in a low Earth orbital environment, that mandates welding. The status of welding technology in the U.S. is assessed.
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: NASA. Lewis Research Center Space Photovoltaic Res. and Technol. 1983; p 220-222
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  • 82
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    In:  CASI
    Publikationsdatum: 2006-02-14
    Beschreibung: Anchorage dependent cell cultures in fluidized beds are tested. Feasibility calculations indicate the allowed parameters and estimate the shear stresses therein. In addition, the diffusion equation with first order reaction is solved for the spherical shell (double bubble) reactor with various constraints.
    Schlagwort(e): FLUID MECHANICS AND HEAT TRANSFER
    Materialart: Houston Univ. The 1981 NASA ASEE Summer Fac. Fellowship Program, Vol. 2; 19 p
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  • 83
    Publikationsdatum: 2006-02-14
    Beschreibung: Solid rocket booster cavity collapse flight measurements included external pressures on the motor case and aft skirt, internal motor case pressures, accelerometers located in the forward skirt, mid-body area, and aft skirt, as well as strain gages located on the skin of the motor case. This flight data yielded applied pressure longitudinal and circumferential distributions which compare well with model test predictions. The internal motor case ullage pressure, which is below atmospheric due to the rapid cooling of the hot internal gas, was more severe (lower) than anticipated due to the ullage gas being hotter than predicted. The structural dynamic response characteristics were as expected. Structural ring and wall damage are detailed and are considered to be attributable to the direct application of cavity collapse pressure combined with the structurally destabilizing, low internal motor case pressure.
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: Shock and Vibration Inform. Center The Shock and Vibration Bull., No. 52. Part 2; p 21-26
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  • 84
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    In:  CASI
    Publikationsdatum: 2006-02-14
    Beschreibung: Transpiration cooling is treated and then full coverage discrete hole injection for three injection orientations. Spacings with pitch to diameter ratios of 5 and 10 are discussed. The array is staggered, with the transverse pitch and the streamwise pitch the same. Results are presented in terms of the Stanton number using the heat transfer coefficient defined in terms of the difference between the wall temperature and the free stream temperature. Two values of Stanton number are provided for each situation: one with the injectant at wall temperature, and the other with the injectant at free stream temperature. These two values are equivalent to knowing the heat transfer coefficient and the adiabatic effectiveness. The heat transfer coefficient thus defined is used with the actual wall temperature to and the actual gas temperature to calculate the heat load. The principle of superposition thus invoked is valid exactly when the governing equations are linear.
    Schlagwort(e): FLUID MECHANICS AND HEAT TRANSFER
    Materialart: Von Karman Inst. for Fluid Dyn. Film Cooling and Turbine Blade Heat Transfer, Vol. 1; 27 p
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  • 85
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    In:  CASI
    Publikationsdatum: 2006-04-25
    Beschreibung: NASA computer program for dynamic structural analysis in stress and thermal deformation problems
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: NIFICANT ACCOMPLISHMENTS IN SCI. AND TECHNOL. AT GODDARD SPACE FLIGHT CENTER 1970; P 221-224
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  • 86
    Publikationsdatum: 2006-02-14
    Beschreibung: Researchers define damage-tolerant structural systems as those systems which not only have adeqate intact strength to withstand initial failure but also adequate residual strength to minimize the possibility of, and hence the consequences of, further failure. The incorporation of damage tolerance cannot be done in total isolation of the function being required of the system and the costs associated with obtaining improved damage tolerance. The approach, therefore, is to formulate multiple-objective, multi-level decision support problems (DSP), the solutions of which represent a compromise between higher costs and higher damage tolerance. Mulitple-objective decision support problems are easily solved in the linear domain. These formulations, however, include both linear and nonlinear constraints and goals, which in the past, have not been considered due to the resulting complexity. Here, researchers: (1) present a complete discussion and description of decision support problems; (2) identify what further research needs to be done in order to obtain information that is required but not known for solving problems using these models; and (3) identify what needs to be done to implement this prototype method in practice.
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: NASA. Langley Research Center Recent Experiences in Multidisciplinary Analysis and Optimization, Part 2; 36 p
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  • 87
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    In:  CASI
    Publikationsdatum: 2006-02-14
    Beschreibung: Ocean-going vehicles and platforms are among the largest structures in the world and are subjected to relatively harsh conditions of motions and loads. Some of them, such as semi-submersible platforms, are a relatively new type of structure and hence there is no formal, well evolved and established structural design code as there is for more traditional structures. More recently, efforts have also been made to develop a design method of this type for ships and other ocean structures. One of the many advantages of a rationally based design method is versatility; it can be used for structures that have widely differing purposes, measures of merit, shapes and sizes. The purpose is to describe a rationally based design method that has been developed within the field of ocean structures, in order that persons dealing with other types of structure can judge whether and to what extent its various features may be useful for those other types. Also, even though some features may not be applicable they might stimulate some useful ideas.
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: NASA. Langley Research Center Recent Experiences in Multidisciplinary Analysis and Optimization, Part 2; 18 p
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  • 88
    Publikationsdatum: 2006-02-14
    Beschreibung: Technical improvements of a long life heat rejection system, suitable for long duration high power missions, that can be constructed and deployed in orbit is discussed. A mathematical model is formulated and a computer program developed which describes the transient priming characteristics of a dual passage heat pipe. An experimental test package is described for flight in the KC-135 Zero-g Aircraft, to be used to verify the modeling predictions.
    Schlagwort(e): FLUID MECHANICS AND HEAT TRANSFER
    Materialart: Houston Univ. The 1981 NASA ASEE Summer Fac. Fellowship Program, Vol. 2; 50 p
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  • 89
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    Unbekannt
    In:  CASI
    Publikationsdatum: 2006-02-14
    Beschreibung: The random vibration of the components of the space shuttle causing internal cargo bay acoustic impingement on the payload was investigated. The import factors to be considered in the design of acoustically loaded structures are the prediction of acoustic environment, prediction of structural response to this environment, and to determine the effect of the response on the structural strength requirements. Two basic responses were analyzed. The primary structure response due to random vibration is first analyzed. The output of primary structure response is used as an input to the secondary structure to calculate the component response.
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: Alabama Univ. in Huntsville The 1981 NASA(ASEE Summer Fac. Fellowship Program; 12 p
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    Standort Signatur Erwartet Verfügbarkeit
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  • 90
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    Unbekannt
    In:  CASI
    Publikationsdatum: 2006-02-14
    Beschreibung: Analysis techniques for three aspects of the performance of the NASA/MSFC 32 meter drop tube are considered. Heat loss through the support wire in a pendant drop sample, temperature history of a drop falling through the drop tube when the tube is filled with helium gas at various pressures, and drag and resulting g-levels experienced by a drop falling through the tube when the tube is filled with helium gas at various pressures are addressed. The developed methods apply to systems with sufficiently small Knudsen numbers for which continuum theory may be applied. Sample results are presented, using niobium drops, to indicate the magnitudes of the effects. Helium gas at one atmosphere pressure can approximately double the amount of possible undercooling but it results in an apparent gravity levels of up to 0.1 g.
    Schlagwort(e): FLUID MECHANICS AND HEAT TRANSFER
    Materialart: the 1981 NASA(ASEE Summer Fac. Fellowship Program; 31 p
    Format: text
    Standort Signatur Erwartet Verfügbarkeit
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  • 91
    Publikationsdatum: 2006-02-14
    Beschreibung: The elastic membrane equations which describe the deflection of a biaxially tensioned reflective mesh from an idealized surface were developed and solved. The conditions of equilibrium of the forces acting on a membrane element furnish equations which may be used to solve a variety of problems. Configurations considered include continuous, as well as incremental mesh attachment to structural members to form shapes which are approximately parabolic or spherical.
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: Alabama Univ. in Huntsville The 1981 NASA(ASEE summer Fac. Fellowship Program; 11 p
    Format: text
    Standort Signatur Erwartet Verfügbarkeit
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  • 92
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    Unbekannt
    In:  CASI
    Publikationsdatum: 2006-02-14
    Beschreibung: Spacelab experiment to investigate two-phase flow patterns under gravity uses a water-air mixture experiment. Air and water are circulated through the system. The quality or the mixture or air-water is controlled. Photographs of the test section are made and at the same time pressure drop across the test section is measured. The data establishes a flow regime map under reduced gravity conditions with corresponding pressure drop correlations. The test section is also equipped with an electrical resistance heater in order to allow a flow boiling experiment to be carried out using Freon II. High-speed photographs of the test section are used to determine flow patterns. The temperature gradient and pressure drop along the duct can be measured. Thus, quality change can be measured, and heat transfer calculated.
    Schlagwort(e): FLUID MECHANICS AND HEAT TRANSFER
    Materialart: NASA. Marshall Space Flight Center Spacecraft Dyn. as Related to Lab. Expt. in Space; p 43-57
    Format: text
    Standort Signatur Erwartet Verfügbarkeit
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  • 93
    facet.materialart.
    Unbekannt
    In:  CASI
    Publikationsdatum: 2006-02-14
    Beschreibung: The equations of motion governing an incompressible fluid contained in an orbiting laboratory were examined to isolate various fictitious forces and their relative influence on the fluid. The forces are divided into those arising from the orbital motions and those arising from small local motions of the spacecraft about its center of mass. The latter dominate the nonrotating experiments. Both are important for rotating experiments. A brief discussion of the onset of time-dependence and violent instability in earth-based rotating and processing systems is given.
    Schlagwort(e): FLUID MECHANICS AND HEAT TRANSFER
    Materialart: NASA. Marshall Space Flight Center Spacecraft Dyn. as Related to Lab. Expt. in Space; p 96-102
    Format: text
    Standort Signatur Erwartet Verfügbarkeit
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  • 94
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    Unbekannt
    In:  CASI
    Publikationsdatum: 2006-02-14
    Beschreibung: Natural convection is not always harmful and, therefore, to be avoided. In some situations it may be desirable to have fluid flows in space processes, e.g., to stir the fluid phase for mixing and cooling or to help maintain concentration gradients. In may event, it is important to know the extent and nature of convection in space and the factors on which it depends, in order either to minimize the effects to convection, or to utilize the convection to advantage. The information needed to assess both conventional and unstable convection includes: (1) the magnitude and direction of accelerations; (2) geometric configuration; (3) imposed boundary conditions; and (4) material properties.
    Schlagwort(e): FLUID MECHANICS AND HEAT TRANSFER
    Materialart: NASA. Marshall Space Flight Center Spacecraft Dyn. as Related to Lab. Expt. in Space; p 69-95
    Format: text
    Standort Signatur Erwartet Verfügbarkeit
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  • 95
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    Unbekannt
    In:  CASI
    Publikationsdatum: 2006-02-14
    Beschreibung: Systematic scaling or dimensional analysis reveals that certain scales of geophysical fluid flows (such as stellar, ocean, and planetary atmosphere circulations) can be accurately modeled in the laboratory using a procedure which differs from conventional engineering modeling. Rather than building a model to obtain numbers for a specific design problem, the relative effects of the significant forces are systematically varied in an attempt to deepen understanding of the effects of these forces. Topics covered include: (1) modeling a large-scale planetary atmospheric flow in a rotating cylindrical annulus; (2) achieving a radial dielectric body force; (3) spherical geophysical fluid dynamics experiments for Spacelab flights; (4) measuring flow and temperature; and (5) the possible effect of rotational or precessional disturbances on the flow in the rotating spherical containers.
    Schlagwort(e): FLUID MECHANICS AND HEAT TRANSFER
    Materialart: Spacecraft Dyn. as Related to Lab. Expt. in Space; p 25-31
    Format: text
    Standort Signatur Erwartet Verfügbarkeit
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  • 96
    Publikationsdatum: 2006-01-11
    Beschreibung: One of the most important methods of reducing the noise and vibration level is the damping of the secondary sources, such as metal plates, often used in vehicle structures, by means of covering materials with high internal viscosity. Damping layers are chosen at an optimum thickness corresponding to the frequency and temperature range in which a certain structure works. The structure's response corresponding to various real situations is analyzed by means of a measuring chain including electroacoustical or electromechanical transducers. The experimental results provide the dependence of the loss factor and damping transmission coefficient as a function of the damping layer thickness or of the frequency for various viscoelastic covering materials.
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: The 4th Natl. Conf. on Acoustics, Vol. 1A (NASA-TT-F-15375); p 246-253
    Format: text
    Standort Signatur Erwartet Verfügbarkeit
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  • 97
    Publikationsdatum: 2006-01-11
    Beschreibung: Vibration sources are described for pneumatic hammers used in the mining industry (pick hammers), in boiler shops (riveting hammers), etc., bringing to light the fact that the principal vibration source is the variation in air pressure inside the cylinder. The present state of the art of vibration control of pneumatic hammers as it is practiced abroad, and the solutions adopted for this purpose, are discussed. A new type of pneumatic hammer with a low noise and vibration level is presented.
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: The 4th Natl. Conf. on Acoustics, Vol. 1A (NASA-TT-F-15375); p 79-84
    Format: text
    Standort Signatur Erwartet Verfügbarkeit
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  • 98
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    In:  CASI
    Publikationsdatum: 2006-01-11
    Beschreibung: Special measures are discussed for calculating, designing and executing a forge hammer foundation, so that the vibrations that occur during its working will not be transmitted to neighboring machinery, workrooms and offices. These vibrations are harmful to the workers near the forge hammer.
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: The 4th Natl. Conf. on Acoustics, Vol. 1A (NASA-TT-F-15375); p 73-78
    Format: text
    Standort Signatur Erwartet Verfügbarkeit
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  • 99
    Publikationsdatum: 2006-01-11
    Beschreibung: Because of the high vibration level occurring during the running of electric locomotives, mechanical defects occur in the control mechanisms of auxiliary services. This fact has given rise to the necessity of determining the values of these vibrations in electric locomotives during their running. Measurements were conducted on the Craiova-Drobeta-Turnu Severin line, and measures to reduce the vibration level in electric locomotives were instituted.
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: The 4th Natl. Conf. on Acoustics, Vol. 1A (NASA-TT-F-15375); p 50-54
    Format: text
    Standort Signatur Erwartet Verfügbarkeit
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  • 100
    Publikationsdatum: 2006-01-11
    Beschreibung: A method is presented of determining the mean square transversal deflection of an isotropic and homogeneous linear viscoelastic beam having a certain number of lengthwise distributed lumped masses. It is assumed that the beam is acted upon by a stationary random process uniformly distributed along the beam. The method is useful in vibration level control by means of additional lumped masses.
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: The 4th Natl. Conf. on Acoustics, Vol. 1A (NASA-TT-F-15375); p 36-42
    Format: text
    Standort Signatur Erwartet Verfügbarkeit
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