1–50 von 85 Ergebnissen
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    A General and Extensible Unstructured Mesh Adjoint Method

    Chad Burdyshaw / W. Anderson | AIAA | 2005

    Intermediate altitude rocket exhaust plumes

    ANDERSON, E. W. | AIAA | 1971

    Airfoil Design on Unstructured Grids for Turbulent Flows

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

    Vibration of a cantilever subjected to a tensile follower force.

    ANDERSON, J. M. / KING, W. W. | AIAA | 1969

    Geometric optimization in presence of contact singularities

    Park, Jungsun / Anderson, W. J. | AIAA | 1995

    Natural vibration and buckling of general periodic lattice structures

    ANDERSON, M. S. / WILLIAMS, F. W. | AIAA | 1986

    Blunt-body integral method for air in thermodynamic equilibrium

    ANDERSON, W. A. / XERIKOS, J. | AIAA | 1965

    Thermal Decomposition of Hydrogen Peroxide, Part 2: Modeling Studies

    J. Corpening / S Heister / W. Anderson et al. | AIAA | 2006

    Optimal trajectories of high-thrust aircraft

    ANDERSON, G. M. / OTHLING, W. L. | AIAA | 1976

    Comparison of finite volume flux vector splittings for the Euler equations

    ANDERSON, W. K. / THOMAS, J. L. / VAN LEER et al. | AIAA | 1986

    Investigation of natural frequencies and mode shapes of buckled beams

    Nayfeh, A. H. / Kreider, W. / Anderson, T. J. | AIAA | 1995

    Thermal Decomposition of Hydrogen Peroxide, Part I: Experimental Results

    Jong Soo Mok / W Helms / James Sisco et al. | AIAA | 2005

    Analytical Approximation for the Mechanics of Airplane Spin

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

    Step-Size Independent Approach for Multidisciplinary Sensitivity Analysis

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

    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

    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

    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

    Axisymmetric nose inlet effects on supersonic airloads

    FINK, M. R. / ANDERSON, W. E. | AIAA | 1983

    Mode tracking issues in structural optimization

    Eldred, M. S. / Venkayya, V. B. / Anderson, W. J. | AIAA | 1995

    Multigrid acceleration of the flux-split Euler equations

    ANDERSON, W. KYLE / THOMAS, JAMES L. / WHITFIELD, DAVID L. | AIAA | 1988