1–20 von 79 Ergebnissen
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    Aerothermal Environment for Hypersonic Vehicle Design Current Practices and Future Requirements

    Venkatapathy, E. | British Library Conference Proceedings | 1999

    ADEPT for Secondary Payloads

    Smith, B. / Cassell, A. / Venkatapathy, E. | NTRS | 2014

    Flow structure capturing on overset patched meshes

    VENKATAPATHY, E. / LOMBARD, C. | AIAA | 1985

    Numerical solution of supersonic viscous flow over blunt delta wings

    TANNEHILL, J. / VENKATAPATHY, E. / RAKICH, J. | AIAA | 1981

    Universal single level implicit algorithm for gasdynamics

    LOMBARD, C. / VENKATAPATHY, E. / BARDINA, J. | AIAA | 1984

    Numerical solution of Space Shuttle Orbiter flow field

    VENKATAPATHY, E. / TANNEHILL, J. / RAKICH, J. | AIAA | 1982

    Design and Analysis of an Ellipsoid-Paraboloid Aerobrake for Near-Earth Commercial Missions

    Venkatapathy, E. / Park, C. / AIAA | British Library Conference Proceedings | 1994

    AOTV bluff body flow - Relaxation algorithm

    LOMBARD, C. / BARDINA, J. / VENKATAPATHY, E. | AIAA | 1984

    Design and Analysis of an Ellipsoid-Paraboloid Aerobrake for Near-Earth Commercial Missions

    Venkatapathy, E. / Park, C. / AIAA | British Library Conference Proceedings | 1994

    Thermal Protection System Technology and Facility Needs for Demanding Future Planetary Missions

    Laub, B. / Venkatapathy, E. / European Space Agency | British Library Conference Proceedings | 2004

    Thermal protection system development, testing, and qualification for atmospheric probes and sample return missions

    Examples for Saturn, Titan and Stardust-type sample return
    Venkatapathy, E. / Laub, B. / Hartman, G.J. et al. | Elsevier | 2008

    Hypersonic combustor model inlet CFD simulations and experimental comparisons

    Venkatapathy, E / Tokarcik-Polsky, S / Deiwert, G | AIAA | 1995

    Enabling Entry Technologies for Ice Giant Missions

    Venkatapathy, E. / Austin, A. / Cassell, A. et al. | NTRS | 2020