41–60 von 1,571 Ergebnissen
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    Velocity effects on a body passing through a rocket plume.

    DRAPER, J. S. / HILL, J. A. F. / JARVINEN, P. O. | AIAA | 1968

    Velocity and thrust measurements in a quasi- steady magnetoplasmadynamic thruster

    BURLOCK, J. / HOELL, JR., J. / JARRETT, JR., O. | AIAA | 1970

    Valve without external shaft

    Meyer, F. / Faye, O. | AIAA | 1999

    Validation of the Uranus Navier-Stokes code for high-temperature nonequilibrium flows

    Daiss, A. / Schoell, E. / Fruehauf, H.-H. et al. | AIAA | 1993

    Validation of a finite element error estimator

    DOW, J. O. / HARWOOD, S. A. / JONES, M. S. et al. | AIAA | 1991

    Utilizing air-turborocket and rocket propulsion for a single-stage-to-orbit vehicle

    LEPSCH, ROGER A. / STANLEY, DOUGLAS O. / CRUZ, CHRISTOPHER I. et al. | AIAA | 1991

    User-friendly codes for heat transfer calculations

    Torella, G. / Romano, F. / Manca, O. | AIAA | 1998

    USE OF RF BRIDGE FOR REENTRY PLASMA DIAGNOSTICS

    FUHS, A. / GRABOWSKY, W. / GIBB, O. | AIAA | 1966

    Use of an expansion tube to examine scramjet combustion at hypersonic velocities

    RIZKALLA, O. / BAKOS, R. / PULSONETTI, M. et al. | AIAA | 1989

    Use of a deformable core vortex model in predicting vortex-surface interaction

    Radcliff, T. / Burggraf, O. / Conlisk, A. | AIAA | 1999

    Upwind parabolized Navier-Stokes code for chemically reacting flows

    TANNEHILL, JOHN C. / IEVALTS, JOHN O. / BUELOW, PHILIP E. et al. | AIAA | 1990