1–20 von 21 Ergebnissen
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    Aerodynamic heating to the hypersonic research aircraft, X-24C

    NEUMANN, R. / PATTERSON, J. / SLISKI, N. | AIAA | 1978

    Minimizing boundary layer bleed for a mixed compression inlet

    WASSERBAUER, J. / SHAW, R. / NEUMANN, H. | AIAA | 1973

    Aero thermodynamic and configuration development

    ANTONATOS, P. / DRAPER, A. / NEUMANN, R. | AIAA | 1970

    Experimental validation of a grid erosion simulation

    Tartz, M. / Hartmann, E. / Deltschew, R. et al. | AIAA | 1999

    Dynamic distortion in a short s-shaped subsonic diffuser with flow separation

    STUMPF, R. / NEUMANN, H. / GIAMATI, C. | AIAA | 1983

    Reduced gravity experiment capabilities of NASA Lewis' DC-9 aircraft

    McKnight, R. / Neumann, E. / Withrow, J. | AIAA | 1996

    Intermittency in a highly accelerated boundary layer

    BOLDMAN, D. R. / NEUMANN, H. E. | AIAA | 1970

    Grid erosion study of a three-grid ion thruster

    Tartz, M. / Hartmann, E. / Deltschew, R. et al. | AIAA | 1998

    Effect of the plasma inhomogeneity on grid performance

    Tartz, M. / Deltchev, R. / Hartmann, E. et al. | AIAA | 2000

    Redeposition of sputtered material on ion thruster grids

    Deltchev, R. / Tartz, M. / Hartmann, E. et al. | AIAA | 2000

    Ion Analytical Characterisation of the RIT 22 Ion Thruster

    Scholze, Frank / Tartz, Michael / Neumann, Horst et al. | AIAA | 2007

    The development of a generalized advanced propeller analysis system

    GLATT, L. / KOSMATKA, J. / SWIGART, R. et al. | AIAA | 1983