1–20 von 71 Ergebnissen
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    Solar simulation testing of the nuclear test detection spacecraft

    GLENN, E. / GOLDMAN, K. / LEHR, S. et al. | AIAA | 1964

    A study of heterogeneous detonations

    RAGLAND, K. / DABORA, E. / NICHOLLS, J. | AIAA | 1966

    Supersonic dynamic stability experiments on the space shuttle

    ORLIK-RUECKEMANN, K. / LABERGE, J. / HANFF, E. | AIAA | 1972

    Measurement of dynamic cross-derivatives due to pitching and yawing

    ORLIK-RUECKEMANN, K. / LABERGE, J. / HANFF, E. | AIAA | 1974

    V/STOL demonstrator vehicle for ejector thrust augmentation technology

    BYRNES, J. / MURPHY, R. / BALL, R. et al. | AIAA | 1974

    Turbulent viscous-shock-layer solutions with strong vorticity interaction

    ANDERSON, E. / MOSS, J. / SUTTON, K. | AIAA | 1976

    Application of skin technology to turbine blades

    WORTMANN, J. / SCHWEITZER, K. / SPRENGER, H. et al. | AIAA | 1978

    Approximate convective heating equations for hypersonic flows

    ZOBY, E. / MOSS, J. / SUTTON, K. | AIAA | 1979

    Downstream mixing gasdynamic lasers - A numerical solution

    PARTHASARATHY, K. / ANDERSON, JR., J. / JONES, E. | AIAA | 1979

    Heat pipe avionic thermal control

    TOKEN, K. / GARNER, E. / COOK, R. et al. | AIAA | 1980

    Laminar boundary layer stability experiments on a cone at Mach 8. I - Sharp cone

    STETSON, K. / THOMPSON, E. / DONALDSON, J. et al. | AIAA | 1983

    Recession behavior of graphitic nozzles in simulated rocket motors

    KESWANI, S. / ANDIROGLU, E. / CAMPBELL, J. et al. | AIAA | 1983

    Design and performance evaluation of a two-position variable geometry turbofan combustor

    SANBORN, J. / SCHEIHING, P. / COLEMAN, E. et al. | AIAA | 1984

    Total pressure loss in vortical solutions of the conical Euler equations

    POWELL, K. / MURMAN, E. / PEREZ, E. et al. | AIAA | 1985