1–50 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

    A multiblock approach for calculating incompressible fluid flows on unstructured grids

    Sheng, Chunhua / Whitfield, David / Anderson, W. | AIAA | 1997

    Analysis and Design of Solid Oxide Fuel Cells with Advanced Numerical Techniques

    Elliott, Louie / Anderson, W. / Kapadia, Sagar et al. | AIAA | 2007

    Analysis and Experiments of Hydrogen Peroxide Vaporization and Decomposition

    Mok, J. S. / Sisco, J. / Anderson, W. | AIAA | 2003

    Analytical Approximation for the Mechanics of Airplane Spin

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

    An Evaluation of Ablation Mechanisms for the Apollo Heat Shield Material

    EUGENE P. BARTLETT / LARRY W. ANDERSON AND DONALD M. CURRY | AIAA | 1971

    An MDO approach to Control-Configured-Vehicle design

    Anderson, M. / Mason, W. | AIAA | 1996

    Annular Suspension and Pointing System

    Willard W. Anderson / Nelson J. Groom / Charles T. Woolley | AIAA | 1979

    An O(Nm2) plane solver for the compressible Navier-Stokes equations

    Thomas, J. / Bonhaus, D. / Anderson, W. et al. | AIAA | 1999

    Application of an upwind Navier-Stokes code to two-dimensional transonic airfoil flow

    RUMSEY, CHRISTOPHER / THOMAS, JAMES / ANDERSON, W. | AIAA | 1987

    Application of Newton-Krylov methodology to a three-dimensional unstructured Euler code

    Nielsen, Eric / Walters, Robert / Anderson, W et al. | AIAA | 1995

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

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

    Atomization characteristics of impinging liquid jets

    Ryan, H. M. / Anderson, W. E. / Pal, S. et al. | AIAA | 1995

    Atomization characteristics of impinging liquid jets

    RYAN, H. / ANDERSON, W. / PAL, S. et al. | AIAA | 1993

    Axisymmetric nose inlet effects on supersonic airloads

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

    Blunt-body integral method for air in thermodynamic equilibrium

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

    Catalyst development for hydrogen peroxide rocket engines

    Morlan, P. / Wu, P.-K. / Ruttle, D. et al. | AIAA | 1999