1–50 von 258 Ergebnissen
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    High-Lift Aerodynamics

    A. M. O. Smith | AIAA | 1975

    Measurements of test time in the galcit 17-inch shock tube

    ROSHKO, A. / SMITH, J. A. | AIAA | 1964

    Preconditioning applied to variable and constant density flows

    Weiss, Jonathan M. / Smith, Wayne A. | AIAA | 1995

    Passive FuelAir Mixing and Emissions Control Via Lobed Injectors

    M. Mitchell / O. Smith / A. Karagozian | AIAA | 2004

    Passive Mixing Control via Lobed Injectors in High-Speed Flow

    A. J. Majamaki / O. I. Smith / A. R. Karagozian | AIAA | 2003

    Lunar power systems

    SCHULMAN, F. / SMITH, A. | AIAA | 1967

    Secant-method adjustment for structural models

    SMITH, SUZANNE WEAVER / BEATTIE, CHRISTOPHER A. | AIAA | 1991

    Experimental aerodynamics of a rotor entry vehicle

    LEVIN, A. / SMITH, R. | AIAA | 1968

    Measurement of the speed of sound in ice

    SMITH, A. C. / KISHONI, D. | AIAA | 1986

    The Boundary Layer and I

    A. M. O. Smith | AIAA | 1981

    High aspect ratio forward sweep for transport aircraft

    SMITH, P. / SROKOWSKI, A. | AIAA | 1983

    A pressurized deployment model for inflatable space structures

    Clem, A. / Smith, S. / Main, J. | AIAA | 2000

    Emissions measurements from a lobed fuel injector/burner

    Mitchell, M. / Smith, L. / Karagozian, A. et al. | AIAA | 1998

    Acoustical excitation of burning fuel droplets

    Ghenai, C. / Smith, O. / Karagozian, A. | AIAA | 2001

    Deployment dynamics of an inflatable solar array

    Clem, A. / Smith, S. / Main, J. | AIAA | 1999

    H-R/x/ method for predicting transition

    WAZZAN, A. R. / GAZLEY, C. / SMITH, A. M. O. | AIAA | 1981

    VELOCITY DEFECT LAW FOR A TRANSPIRED TURBULENT BOUNDARY LAYER

    MICKLEY, H. S. / SMITH, K. A. | AIAA | 1963

    Optimal pulse motor control

    CALISE, A. / SMITH, S. | AIAA | 1982