1–20 von 32 Ergebnissen
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    Modified Mode-I cracked sandwich beam (CSB) fracture test

    Smith, S. / Shivakumar, K. | AIAA | 2001

    A pressurized deployment model for inflatable space structures

    Clem, A. / Smith, S. / Main, J. | AIAA | 2000

    Dynamic behavior of a cylinder with a cutout.

    BROGAN, F. / FORSBERG, K. / SMITH, S. | AIAA | 1969

    Deployment dynamics of an inflatable solar array

    Clem, A. / Smith, S. / Main, J. | AIAA | 1999

    The design of a joined wing flight demonstrator aircraft

    SMITH, S. / CLIFF, S. / KROO, I. | AIAA | 1987

    Simulation of atmospheric turbulent gusts and gust gradients

    TATOM, F. / SMITH, S. / FICHTL, G. | AIAA | 1981

    Parametric response of thin beams and film strips in a vacuum

    Vulkarni, V. / Smith, S. / Main, J. | AIAA | 2001

    Simulation of dynamic loads by multichannel digital control

    HAMMA, G. / SMITH, S. / STROUD, R. | AIAA | 1978

    Radiation-conduction interaction in large space structures

    EMERY, A. / MORTAZAVI, H. / SMITH, S. | AIAA | 1984

    Post-flight testing and analysis of zero-gravity deployment of an inflating tube

    Smith, S. / Elliott, M. / Main, J. et al. | AIAA | 2001