1–20 von 179 Ergebnissen
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    A comparison of finite volume flux vector splittings for the Euler equations

    ANDERSON, W. / THOMAS, J. / VAN LEER, B. | AIAA | 1985

    Acoustic Mode Simulations in Experimental Rocket Combustors

    Ellis, M. / Xia, Guoping / Sankaran, V. et al. | AIAA | 2005

    Added mass of high-altitude balloons

    ANDERSON, W. | AIAA | 1991

    Added mass of high-altitude balloons

    Anderson, W. J. / Shah, G. N. / Park, Jungsun | AIAA | 1995

    Advanced mass memories

    SCHWEE, L. / ANDERSON, W. / LIU, Y. et al. | AIAA | 1977

    A facility for active flow control research in serpentine inlets

    Rabe, A. / Olcmen, S. / Anderson, J. et al. | AIAA | 2002

    A General and Extensible Unstructured Mesh Adjoint Method

    Chad Burdyshaw / W. Anderson | AIAA | 2005

    A General and Extensible Unstructured Mesh Adjoint Method

    Burdyshaw, Chad / Anderson, W. Kyle | AIAA | 2005

    Air data estimation system for control of guided munitions

    ANDERSON, M. / LAWRENCE, W. / LOPEZ, J. | AIAA | 1993

    Air data prediction from surface pressure measurements on guided munitions

    Anderson, M. B. / Lawrence, W. R. / Lopez, J. L. | AIAA | 1995

    Airfoil Design on Unstructured Grids for Turbulent Flows

    W. Kyle Anderson / Daryl L. Bonhaus | AIAA | 1999

    Air-to-Air Missile Trajectories for Maximization of Launch Range

    GERALD M. ANDERSON AND GEORGE W. WATT | AIAA | 1971

    Alleviation of Spin-Entry Tendencies through Localization of Wing-Flow Separation

    T. W. Feistel / S. B. Anderson / R. A. Kroeger | AIAA | 1981

    A method of order reduction for structural dynamics

    ANDERSON, L. / HALLAUER, JR., W. | AIAA | 1980