1–20 von 31 Ergebnissen
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    AN AUTOMATED METHOD OF COMPUTING AEROELASTIC BODY LOADS

    ARNOLD, R. / TAYLOR, J. / MAUN, E. | AIAA | 1967

    Optimal Quasi-Steady Plasma Thruster System Characteristics

    DENNIS E. LUDWIG AND ARNOLD J. KELLY | AIAA | 1973

    Normal shock-wave properties in imperfect air and nitrogen

    BURGESS, E. G. / ARO, INC. / ARNOLD ENGINEERING DEVELOPMENT CENTER et al. | AIAA | 1965

    Altitude-velocity charts for imperfect air

    BURGESS, E. G. / ARO, INC. / ARNOLD ENGINEERING DEVELOPMENT CENTER et al. | AIAA | 1965

    Calibration and use of electrostatic probes for hypersonic wake studies

    APPLETON, J. P. / ARNOLD, T. E. / FRENCH, I. P. et al. | AIAA | 1970

    Experiments on a Faraday-type MHD accelerator with series-connected electrodes.

    RITTENHOUSE, L. E. / TEMPELMEYER, K. E. | AIAA | 1965

    Near- and farfield measurements of aero-optical effects due to propagation through hypersonic flows

    Yanta, William / Sprin, Charles / Lafferty, John et al. | AIAA | 2000

    Supersonic cone wake-neck geometry.

    KOCH, K. E. | AIAA | 1967

    Lightning and related phenomena in isolated thunderstorms and squallline systems

    RUST, W. D. / TAYLOR, W. L. / MACGORMAN, D. R. et al. | AIAA | 1985