1–20 von 200 Ergebnissen
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    Broadband Shock Noise from Supersonic Jets

    T. D. Norum / J. M. Seiner | AIAA | 1982

    INSULATION REQUIREMENTS FOR LONG-TIME LOW-HEAT RATE ENVIRONMENTS

    SHEPPARD, T. D. / TELLEP, D. M. | AIAA | 1963

    Alleviation of the subsonic pitch-up of delta wings

    RAO, D. M. / JOHNSON, T. D. | AIAA | 1983

    Acoustic characteristics of two hybrid inlets at forward speed

    FALARSKI, M. D. / MOORE, M. T. | AIAA | 1980

    Boundary layer transition in hypersonic flows

    MALIK, M. / ZANG, T. / BUSHNELL, D. | AIAA | 1990

    Control law synthesis for an airplane with relaxed static stability

    BLIGHT, J. D. / GANGSAAS, D. / RICHARDSON, T. M. | AIAA | 1986

    Time Domain Nonlinear Aeroelastic Analysis for HALE Wings

    Wang, Zhicun / Chen, P. C. / Liu, D. D. et al. | AIAA | 2006

    Saturn V guidance, navigation, and targeting.

    MARTIN, D. T. / OBRIEN, R. M. | AIAA | 1967

    Spectral methods for the Euler equations. II - Chebyshev methods andshock fitting

    HUSSAINI, M. Y. / KOPRA, D. A. / SALAS, M. D. et al. | AIAA | 1985

    Tailored Dynamic Gain-Scheduled Control

    C. D. C. Jones / M. H. Lowenberg / T. Richardson | AIAA | 2006

    Population inversions behind normal shock waves

    ANDERSON, J. D. / MADDEN, M. T. | AIAA | 1971