1–20 von 45 Ergebnissen
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    Vacuum-air missile boost system

    KUMAR, S. / MURRAY, J. J. / RAJAN, J. R. N. | AIAA | 1964

    Comment on Rates of Change of Flutter Mach Number and Flutter Frequency

    KUMAR G. BHATIA AND CARL S. RUDISILL | AIAA | 1973

    Thermal Conductivity of Comets

    G. N. Kumar / M. S. Khader / R. I. Vachon | AIAA | 1975

    Laminar and turbulent flow solutions with radiation and ablation injection for Jovian entry

    KUMAR, A. / TIWARI, S. / GRAVES, JR., R. et al. | AIAA | 1980

    Inclination correction for geostationary orbits using ion thrusters

    KUMAR, S. P. / KUDVA, P. / GOEL, P. S. | AIAA | 1985

    Numerical study of supersonic combustion using a finite rate chemistry model

    CHITSOMBOON, T. / TIWARI, S. / KUMAR, A. et al. | AIAA | 1986

    Numerical study of finite-rate supersonic combustion using parabolized equations

    CHITSOMBOON, T. / KUMAR, A. / TIWARI, S. | AIAA | 1987

    Transient radiative energy transfer in nongray gases

    TIWARI, S. / SINGH, D. / KUMAR, A. | AIAA | 1987

    Spin rate variations of spin-stabilized apogee motors in thrust phase

    ADIMURTHY, V. / KUMAR, PRADEEP / LAKSHMINARAYANAN, S. | AIAA | 1988

    Three-dimensional shock-shock interactions on the scramjet inlet

    SINGH, D. / TIWARI, S. / KUMAR, A. | AIAA | 1990

    Minimum fuel spacecraft reorientation

    Seywald, Hans / Kumar, Renjith R. / Deshpande, Samir S. et al. | AIAA | 1994