1–20 von 41 Ergebnissen
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    An Analytical Model for Nitric Oxide Formation in a Gas Turbine Combustor

    RICHARD ROBERTS / LEONARD D. ACETO / REINER KOLLRACK et al. | AIAA | 1972

    New directions in automated spacecraft cost estimation

    PEKAR, P. P. / FRIEDLANDER, A. L. / ROBERTS, D. L. | AIAA | 1975

    An analytical method for ride quality of flexible airplanes

    SWAIM, R. L. / SCHMIDT, D. K. / ROBERTS, P. A. et al. | AIAA | 1977

    The stability of a tethered gyromill

    RYE, D. / ROBERTS, B. | AIAA | 1981

    Rocket exhaust plume induced flowfield interaction experiences with the Space Shuttle

    ROBERTS, B. / WALLACE, R. / CRAIG, M. et al. | AIAA | 1983

    The concept of lateral blowing

    TAVELLA, D. / ROBERTS, L. | AIAA | 1985

    A zonal computational approach to thrust augmentor optimization

    LUND, T. / TAVELLA, D. / ROBERTS, L. | AIAA | 1985

    An investigation of film cooling on a hypersonic vehicle using a PNSflow analysis code

    BANKEN, G. / ROBERTS, D. / HOLCOMB, J. et al. | AIAA | 1985

    Analysis of interacting dual lifting ejector systems

    LUND, T. / TAVELLA, D. / ROBERTS, L. | AIAA | 1986

    Flow structure of lateral wing-tip blowing

    LEE, C. / TAVELLA, D. / WOOD, N. et al. | AIAA | 1986

    The jet spoiler as a yaw control device

    TAVELLA, D. / LEE, C. / WOOD, N. et al. | AIAA | 1986

    Thrust augmentor inlet optimization

    LUND, T. S. / TAVELLA, D. A. / ROBERTS, L. | AIAA | 1986