1–20 of 8,351 hits
|

    Comparison of integrally formed compression panel efficiencies with other aerospace panel concepts

    McClaren, S.W. / McQueen, J.C. / Martin, A.P. | Engineering Index Backfile | 1967
    Examples of structures include conventional sheet-stringer panels, honeycomb panels, integrally machined and stiffened panels, trusscore ...
    Keywords: Rockets and missiles

    Status of reentry vehicle heatshields

    Channon, S.L. / Barry, W.T. | Engineering Index Backfile | 1967
    influence selection of materials for heat shield application are vehicle configuration, ballistic coefficient, re-entry velocity and flight ...

    Optimal control of maneuver-induced vibration in flexible aerospace vehicles

    Karnopp, D. | Engineering Index Backfile | 1967
    ; some typical thrust patterns are examined which accomplish desired maneuver and also are constrained to leave some vibratory modes unexcited at ...

    AIAA/ASME 9th structures, structural dynamics and materials conference

    Engineering Index Backfile | 1968
    Twenty-four papers deal with applications in fields of aerospace vehicle design and shell structures; individual papers are abstracted ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA)
    Keywords: Structural design

    Material design concepts for urban transport aircraft

    MacNeill, C.E. | Engineering Index Backfile | 1968
    fracture toughness, creep, and fatigue properties; composite materials offer improved service use by providing freedom from deterioration and ease ...
    Keywords: Aircraft materials

    Response of aerospace vehicle skin panels to oscillating shock waves

    Crocker, M.J. | Engineering Index Backfile | 1968
    one panel with arbitrary edge constraints to shock wave oscillating at discrete frequency and to shock wave moving with constant velocity; it ...

    Volume of technical papers on structural dynamics

    Structures, Structural Dynamics and Materials Conference / Structural Dynamics and Aeroelasticity Specialist Conference / American Institute of Aeronautics and Astronautics et al. | TIBKAT | 1969
    Publisher: American Institute of Aeronautics and Astronautics , New York, NY

    AIAA Structural Dynamics and Aeroelasticity Specialist Conference : New Orleans, Louisiana, April 16 - 17, 1969

    Structural Dynamics and Aeroelasticity Specialist Conference / American Institute of Aeronautics and Astronautics | TIBKAT | 1969
    Publisher: American Institute of Aeronautics and Astronautics , New York

    Applications of space developments, the 31st int. astronautical cong., Proc., Sept. 21- 28, 1980, Tokyo, J, (Part 4)

    Tema Archive | 1981
    deployable and erectable spacecraft (179-198). -- Garibotti, J.F.: Material and structural approaches for large space structures (199-212 ...

    A collection of technical papers // AIAA/ASME/ASCE/AHS 28th Structures, Structural Dynamics, and Materials Conference, April 6 - 8, 1987, Monterey, California / [General chairman: Keith T. Kedward] ; Pt. 2B: AIAA/ASME/ASCE/AHS Structures, Structural Dynamics, and Materials Conference and AIAA Dynamics Specialists Conference : Monterey, California, April 9 - 10, 1987

    Structures, Structural Dynamics, and Materials Conference / Dynamics Specialists Conference / American Institute of Aeronautics and Astronautics et al. | TIBKAT | 1987
    Publisher: American Institute of Aeronautics and Astronautics , Washington, DC

    A collection of technical papers // AIAA/ASME/ASCE/AHS 28th Structures, Structural Dynamics, and Materials Conference, April 6 - 8, 1987, Monterey, California / [General chairman: Keith T. Kedward] ; Pt. 2A: AIAA/ASME/ASCE/AHS Structures, Structural Dynamics, and Materials Conference and AIAA Dynamics Specialists Conference : Monterey, California, April 9 - 10, 1987

    Structures, Structural Dynamics, and Materials Conference / Dynamics Specialists Conference / American Institute of Aeronautics and Astronautics et al. | TIBKAT | 1987
    Publisher: American Institute of Aeronautics and Astronautics , Washington, DC

    A structural design and optimization tool for ducted rotor/wing blades

    Crossley, W.A. / Laananen, D.H. / Rutherford, J.W. | Tema Archive | 1992
    tool, a minimum weight blade design can be found. Optimization of the blade is carried out varying the thickness of structural components in ...

    A study on the feasibility of using adaptive structures in the attenuation of vibration characteristics of rotary wings

    Nitzsche, F. / Breitbach, E. | Tema Archive | 1992
    This paper investigates the feasibility of employing adaptive material to build both sensors and actuators to attenuate the higher harmonic ...

    Combined compressive and shear buckling analysis of hypersonic aircraft sandwich panel

    Ko, W.L. / Jackson, R.H. | Tema Archive | 1992
    The combined-load (compression and shear) buckling equations were established for orthotropic sandwich panels by using the Rayleigh-Ritz ...

    Aeroelastic response and blade loads ofa composite rotor in forward flight

    Smith, E.C. / Chopra, I. | Tema Archive | 1992
    related warping and inplane elasticity is integrated with the University of Maryland Advanced Rotorcraft Code (UMARC). The structural dynamics ...

    Experimental and theoretical study for nonlinear aeroelastic behavior of a flexible rotor blade

    Tang, D.M. / Dowell, E.H. | Tema Archive | 1992
    geometrical and freeplay structural nonlinearity. The ONERA stall aerodynamic model is used. External excitations are provided by base harmonic ...