1–20 von 70 Ergebnissen
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    Starting characteristics of supersonic inlets

    Van Wie, D. / Kwok, F. / Walsh, R. | AIAA | 1996

    Measurement of mass flow in hypersonic facilities

    VAN WIE, D. / WALSH, R. / MCLAFFERTY, G. | AIAA | 1992

    MHD Control of the Separation Phenomenon in a Supersonic Xenon Plasma Flow II

    Bobashev, Sergei / Mende, N. / Sakharov, V. et al. | AIAA | 2004

    Magnetohydrodynamic Influence on a Supersonic Nitrogen Flow About a Body of Revolution

    Bobashev, Sergey / Mende, N. / Sakharov, V. et al. | AIAA | 2007

    Rationale for Ground Test Development of Scramjet Inlets

    Ault, D. / Van Wie, D. / AIAA | British Library Conference Proceedings | 1994

    Rationale for Ground Test Development of Scramjet Inlets

    Ault, D. / Van Wie, D. / AIAA | British Library Conference Proceedings | 1994

    Shock wave characteristics measured in gas discharges

    Van Wie, D. / Wesner, A. / Gauthier, Jr., L. | AIAA | 1999

    A unified methodology for simulation of aerothermochemistry at gas/solid interfaces

    Cybyk, B. / Hunter, L. / Drewry, D. et al. | AIAA | 2002

    Application of CAE and CFD techniques to a complete tactical missiledesign

    BILLIG, F. / WHITE, M. / VAN WIE, D. | AIAA | 1984

    Performance Analysis of Hypersonic Shape-Changing Inlets Derived from Morphing Streamline Traced Flowpaths

    Taylor, T. / Van Wie, D. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2008

    Plasma assisted combustion

    Klimov, A. / Byturin, V. / Brovkin, V. et al. | AIAA | 2001