21–40 von 310 Ergebnissen
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    Non-equilibrium radiation from viscous chemically reacting two-phaseexhaust plumes

    PENNY, M. / SMITH, S. / MIKATARIAN, R. et al. | AIAA | 1976

    An evaluation of excitation and analyses methods for modal testing

    Hamma,G. / Smith,S. / Stroud,R.C. et al. | Kraftfahrwesen | 1976

    Simulation of dynamic loads by multichannel digital control

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

    Summary of solid rocket motor plume flow field and radiation analyses

    Audeh, B. J. / Carter, R. E. / Smith, S. D. | NTRS | 1980

    Lift-enhancing surfaces on several advanced V/STOL fighter/attack aircraft concepts

    DURSTON, D. / SMITH, S. | AIAA | 1981

    Simulation of atmospheric turbulent gusts and gust gradients

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

    Optimal pulse motor control

    CALISE, A. / SMITH, S. | AIAA | 1982

    Exhaust-Plume Impingement Characteristics

    Smith, S. D. / Wojciehowski, C. J. | NTRS | 1983

    Radiation-conduction interaction in large space structures

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

    Simulating Atmospheric Turbulence

    Tatom, F. B. / Smith, S. R. | NTRS | 1984

    The design of a joined wing flight demonstrator aircraft

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

      The design of a joined wing flight demonstrator aircraft

      Smith, S. C. / Cliff, S. E. / Kroo, I. M. | NTRS | 1987