1–7 of 7 hits
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    Synthesis of structural damping.

    Bieber, R. E. / Chang, C. S. | NTRS | 1968
    Force deflection relationship under arbitrary loading for structure exhibiting hysteresis behavior ...
    Keywords: Structural Mechanics

    The European Spacelab structural design evolution

    Thirkettle, A. J. | NTRS | 1982
    low earth orbit in the cargo bay of the Shuttle Transportation System (STS) Orbiter. A description is presented of the structural development ...
    Publisher: NASA National Aeronautics and Space Administration
    Keywords: Spacecraft Design, Testing And Performance

    Recovered transient load analysis for payload structural systems

    Chen, J. C. / Zagzebski, K. P. / Garba, J. A. | NTRS | 1980
    the information on a new payload structure to be launched by an identical launch vehicle. The advantage of the proposed method is that the ...
    Publisher: NASA National Aeronautics and Space Administration
    Keywords: Spacecraft Design, Testing And Performance

    Structural Analysis for the American Airlines Flight 587 Accident Investigation: Global Analysis

    Young, Richard D. / Lovejoy, Andrew E. / Hilburger, Mark W. et al. | NTRS | 2005
    investigation due to LaRC's expertise in high-fidelity structural analysis and testing of composite structures and materials. A Global Analysis Team ...
    Publisher: NASA National Aeronautics and Space Administration
    Keywords: Structural Mechanics

    Structural design of integral tankage for advanced space transportation systems

    Macconochie, I. O. / Davis, R. B. / Lemessurier, R. W. | NTRS | 1982
    large propellant tankage. The dominant structural elements are internal tankage for both cryogenic and non-cryogenic propellants which must ...
    Publisher: NASA National Aeronautics and Space Administration
    Keywords: Spacecraft Design, Testing And Performance

    NASA/FAA general aviation crash dynamics program - A status report

    Thomson, R. G. / Goetz, R. C. | NTRS | 1979
    The objective of the Langley Research Center general aviation crash dynamics program is to develop technology for improved crash safety and ...
    Publisher: NASA National Aeronautics and Space Administration
    Keywords: Aircraft Design, Testing And Performance

    Analysis and Testing of a Composite Fuselage Shield for Open Rotor Engine Blade-Out Protection

    Pereira, J. Michael / Emmerling, William / Seng, Silvia et al. | NTRS | 2015
    new engines that would not have a containment structure on large commercial aircraft. Equivalent safety to the current fleet is desired by the ...
    Publisher: NASA National Aeronautics and Space Administration
    Keywords: Aircraft Design, Testing And Performance , Composite Materials , composite materials