1–50 von 55 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

    A parabolized Navier-Stokes algorithm for separated supersonic internal flows

    CHITSOMBOON, T. / TIWARI, S. / KUMAR, A. | AIAA | 1985

    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

    Comparison of FDNS liquid rocket engine plume computations with SPF/2

    KUMAR, G. / GRIFFITH, II, D. / WARSI, S. et al. | AIAA | 1993

    Minimum fuel spacecraft reorientation

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

    Simulation of shock-induced combustion past blunt projectiles using shock-fitting technique

    Ahuja, J. K. / Tiwari, S. N. / Kumar, A. et al. | AIAA | 1996

    Engine-Airframe Integration During Conceptual Design for Military Application

    Vivek Sanghi / S. Kishore Kumar / V. Sundararajan | AIAA | 1998

    Preliminary Estimation of Engine Gas-Flow-Path Size and Weight

    Vivek Sanghi / S. Kishore Kumar / V. Sundararajan et al. | AIAA | 1998

    Drag Reduction Due to Riblets on a GAW(2) Airfoil

    N. Subaschandar / Rajeev Kumar / S. Sundaram | AIAA | 1999

    Flow prediction in the intermediate casing of compressors

    Narayanan, Vimala / Kumar, S. / Venkatakrishnaiah, T. et al. | AIAA | 2001

    Flow Quality Improvements in a Blowdown Wind Tunnel

    H. Sundara Murthy / R. S. Verma / S. P. Jagadeeswarachar et al. | AIAA | 2001

    Mixing of oxygen and iodine in a subsonic coil

    Kumar, Arvind / Vishwamurthy, S. / Lakhsmi, Srihari et al. | AIAA | 2001

    Assessment of Delamination Fracture Load of Stringer Stiffened Composite Panel

    R. Ramesh Kumar / K. S. Praveen / G. Venkateswara Rao | AIAA | 2003

    Multi-Satellite Scheduling Using Genetic Algorithms

    Soma, P. / Venkateswarlu, S. / Santhalakshmi, S. et al. | AIAA | 2004

    North Star Plasma-Jet Space Experiment

    R. E. Erlandson / P. K. Swaminathan / C. K. Kumar et al. | AIAA | 2004

    Thermophysical Properties Evaluation of High Temperature Resistant Materials by Hot wire Method

    Kesav Kumar, S. / Krishnamoorthy, S. / Subba Rao, S.V. | AIAA | 2006

    Performance of Slanted Entry Nozzle Run by a Supersonic Stream

    Kumar, C. / Elangovan, S. / Lovaraju, P. et al. | AIAA | 2006

    Studies on Internal Flow Choking in Dual-Thrust Motors

    VR Sanal Kumar / BN Raghunandan / HD Kim et al. | AIAA | 2006

    Design and Testing of Clover Nozzle

    Swaraj Kumar, B / Samitha, Z A / Sheena, S et al. | AIAA | 2006

    Fluid-Throat-Induced Shock Waves During the Ignition Transient of Solid Rockets

    Sanal Kumar VR / Heuy-Dong Kim / Raghunandan BN et al. | AIAA | 2006