1–6 von 6 Ergebnissen
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    Using a full potential solver for propulsion system exhaust simulation

    MELVIN, ROBIN G. / JOHNSON, FORRESTER T. / YOUNG, DAVID P. et al. | AIAA | 1993

    The Orbiting Astronomical Observatory thermal test program

    CARUSO, JR., P. / DAN, JR., C. / MENGERS, D. et al. | AIAA | 1969

    Successful Application of New Technologies to the Rosetta and Mars Express Simulations

    Martin, J. E. / Lowe, R. / Osborne, J. J. et al. | AIAA | 2002

    Depressurization induced extinction of burning solid propellant.

    BRUNO, P. S. / GRAESSER, E. C. | AIAA | 1968

    Calculation of Pressures on Bodies at Low Angles of Attack in Supersonic Flow

    F. R. DeJarnette / C. P. Ford / D. E. Young | AIAA | 1980