1–20 von 203 Ergebnissen
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    Comparison of Measurements and Predictions for Blowing from a Turbine Blade Tip

    E. Couch / J. Christophel / E. Hohlfeld et al. | AIAA | 2005

    Quasi-Steady Magnetoplasmadynamic Thruster Performance Database

    E. Y. Choueiri / J. K. Ziemer | AIAA | 2001

    Fluidically Enhanced Chevrons for Supersonic Jet Noise Reduction

    Heeb, N. / Gutmark, E. / Liu, J. et al. | AIAA | 2014

    Simulations of particle dynamics in a confined shear flow

    Chang, E. J. / Kailasanath, K. | AIAA | 1996

    Noncircular jet dynamics in supersonic combustion

    GUTMARK, E. / SCHADOW, K. C. / WILSON, K. J. | AIAA | 1989

    Subsonic and supersonic combustion using noncircular injectors

    GUTMARK, E. / SCHADOW, K. C. / WILSON, K. J. | AIAA | 1991

    Euler calculations for flowfield of a helicopter rotor in hover

    AGARWAL, R. K. / DEESE, J. E. | AIAA | 1987

    Characterization of large-scale structures in a forced ducted flow with dump

    SCHADOW, K. C. / WILSON, K. J. / GUTMARK, E. | AIAA | 1987

    Rearward Forcing of an Unsteady Compressible Cascade

    M. K. Fabian / E. J. Jumper | AIAA | 1999

    Maximum loading capability of axial flow compressors

    SCHWEITZER, J. K. / GARBEROGLIO, J. E. | AIAA | 1984

    Numerical Study of Shock-Reflection Hysteresis in an Underexpanded Jet

    B. J. Gribben / K. J. Badcock / B. E. Richards | AIAA | 2000

    Enhancement of mixing in reacting fuel-rich plumes issued from elliptical nozzles

    SCHADOW, K. C. / WILSON, K. J. / LEE, M. J. et al. | AIAA | 1987

    Microramps Upstream of an Oblique-Shock/Boundary-Layer Interaction

    Lee, S. / Goettke, M. K. / Loth, E. et al. | AIAA | 2010

    Tailored Fuel Injection for Performance Enhancement in a Mach 12 Scramjet Engine

    Barth, James E. / Wise, Dylan J. / Wheatley, Vincent et al. | AIAA | 2015

    In-Space Networking On NASA’s SCaN Testbed

    Brooks, David E. / Eddy, Wesley / Johnson, Sandra K. et al. | AIAA | 2016