61–80 von 129 Ergebnissen
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    Analytical Approximation for the Mechanics of Airplane Spin

    W. F. Phillips / E. A. Anderson | AIAA | 2002

    Hydrogen Peroxide Stability Margin

    Ali, S / Starbuck, T / Anderson, W | AIAA | 2003

    Step-Size Independent Approach for Multidisciplinary Sensitivity Analysis

    David L. Whitfield / James C. Newman / W. Kyle Anderson | AIAA | 2003

    Application of thin-layer Navier-Stokes equations near maximum lift

    ANDERSON, W. / THOMAS, J. / RUMSEY, C. | AIAA | 1984

    Navier-Stokes computations of vortical flows over low-aspect-ratio wings

    THOMAS, JAMES L. / ANDERSON, W. KYLE / KRIST, SHERRIE TAYLOR | AIAA | 1990

    Three-dimensional wake formations behind a family of regular polygonal plates

    Higuchi, H. / Anderson, R. W. / Zhang, J. | AIAA | 1996

    Turbojet exhaust reactions in stratospheric flight

    ANDERSON, L. / MEYER, J. / MCLEAN, W. | AIAA | 1973

    Numerical analysis concepts for balloon analysis

    Anderson, W. / Park, Jungsun / Dungan, Michael | AIAA | 1994

    Predicting the Contribution of Running Propellers to Aircraft Stability Derivatives

    W. F. Phillips / E. A. Anderson / Q. J. Kelly | AIAA | 2003

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

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

    Fundamental studies of impinging liquid jets

    ANDERSON, W. / RYAN, H. / PAL, S. et al. | AIAA | 1992

    Eigenvalue errors in the method of weighted residuals

    ANDERSON, W. J. / CROUCH, J. G. | AIAA | 1970

    Nonlinear inverse perturbation method in dynamic analysis

    ANDERSON, W. J. / SANDSTROM, R. E. / KIM, K.-O. | AIAA | 1983

    Emergency air start system for the F-14B flight test aircraft

    ANDERSON, L. / ENGELMANN, W. / SCICCHITANO, E. | AIAA | 1973

    Development of a reduced mechanism for the double base propellant dark zone

    Ilincic, N. / Seshadri, K. / Anderson, W. | AIAA | 1996