1–20 von 34 Ergebnissen
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    Supersonic Base Flow Problem in Presence of an Exhaust Jet

    Bernhard Wagner / Robert A. White | AIAA | 1980

    Artificial Damping for Spacecraft Structures Based...

    Grillenbeck, A. / Abou-El-Ela, A. / Wagner, M. | AIAA | 2005

    RECENT PROGRESS IN DETONATION RESEARCH

    MANSON, N. / OPPENHEIM, A. K. / WAGNER, H. GG. | AIAA | 1963

    A flight test of laminar flow control leading-edge systems

    FISCHER, M. / WRIGHT, JR., A. / WAGNER, R. | AIAA | 1983

    On the accuracy of modular aeroelastic methods applied to fixed and rotary wings

    Altmikus, A. / Wagner, S. / Hablowetz, Th. et al. | AIAA | 2000

    On-board approach guidance for a planet- orbiter.

    TAYLOR, A. J. / WAGNER, J. T. | AIAA | 1966

    Fluid dynamic studies to M equals 41 in helium

    HENDERSON, JR., A. / WAGNER, JR., R. | AIAA | 1965

    RECENT PROGRESS IN DETONATION RESEARCH AND ITS RELATION TO ROCKET PROPULSION

    OPPENHEIM, A. / MANSON, N. / WAGNER, H. | AIAA | 1963

    Space Operations and Space Station real-time simulation

    HERNANDEZ, D. / MOLINEROS, A. / WAGNER, W. | AIAA | 1988

    Design and test of a propfan gear system

    ANDERSON, N. E. / NIGHTINGALE, L. / WAGNER, D. A. | AIAA | 1989

    Supersonic combustion tests with a double- oblique-shock SCRAMjet ina shock tunnel

    OSGERBY, I. T. / SMITHSON, H. K. / WAGNER, D. A. | AIAA | 1970

    Advanced propfan drive system characteristics and technology needs

    ANDERSON, R. / WAGNER, D. / DEVLIN, R. et al. | AIAA | 1984