101–150 von 179 Ergebnissen
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    Analysis and Experiments of Hydrogen Peroxide Vaporization and Decomposition

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

    Predicting the Contribution of Running Propellers to Aircraft Stability Derivatives

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

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

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

    The Annular Suspension and Pointing System

    ANDERSON, W. / GROOM, N. / WOOLLEY, C. | AIAA | 1978

    Turbojet exhaust reactions in stratospheric flight

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

    Fundamental studies of impinging liquid jets

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

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

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

    Axisymmetric nose inlet effects on supersonic airloads

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

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

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

    Higher order eigenpair perturbations

    ELDRED, M. / ANDERSON, W. / LERNER, P. | AIAA | 1992

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

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

    Nonlinear inverse perturbation method in dynamic analysis

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

    Eigenvalue errors in the method of weighted residuals

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

    Nonlinear incremental inverse perturbation method for structural redesign

    BERNITSAS, M. / SANDSTROM, R. / ANDERSON, W. | AIAA | 1983

    Mode tracking issues in structural optimization

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

    Rotating tests of advanced high temperature wire and thin-film strain gages

    GRANT, H. / ANDERSON, W. / PRZYBYSZEWSKI, J. | AIAA | 1988

    Estimating the low-speed downwash angle on an aft tail

    Phillips, W. / Anderson, E. / Jenkins, J. et al. | AIAA | 2002

    Higher order eigenpair perturbations

    ELDRED, M. S. / LERNER, P. B. / ANDERSON, W. J. | AIAA | 1992

    Multigrid acceleration of the flux-split Euler equations

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

    Added mass of high-altitude balloons

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

    New mode tracking methods in aeroelastic analysis

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

    Transonic Similarity Theory Applied to a Supercritical Airfoil in Heavy Gas

    J. B. Anders / W. K. Anderson / A. V. Murthy | AIAA | 1999

    VICONOPT - Program for exact vibration and buckling analysis or design of prismatic plate assemblies

    WILLIAMS, F. W. / KENNEDY, D. / ANDERSON, M. S. et al. | AIAA | 1991

    Extension and application of flux-vector splitting to calculations on dynamic meshes

    ANDERSON, W. KYLE / THOMAS, JAMES L. / RUMSEY, CHRISTOPHER L. | AIAA | 1989

    A facility for active flow control research in serpentine inlets

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

    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

    Observation of electric fields, electron densities and temperature from the Space Shuttle

    SMIDDY, M. / SULLIVAN, W. / GIROUARD, D. et al. | AIAA | 1983

    Sensitivity Analysis for NavierStokes Equations on Unstructured Meshes Using Complex Variables

    W. Kyle Anderson / James C. Newman / David L. Whitfield et al. | AIAA | 2001

    Flight manifesting process for NASA Microgravity payloads

    Matisak, B. / Ramage, W. / Anderson, S. et al. | AIAA | 2001

    Air data prediction from surface pressure measurements on guided munitions

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

    Acoustic Mode Simulations in Experimental Rocket Combustors

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

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

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

    High temperature, thermally stable JP fuels - An overview

    EDWARDS, T. / ANDERSON, S. / PEARCE, J. et al. | AIAA | 1992

    Long-Life Bipropellant System Demonstration, Viking Orbiter Propulsion System

    D. D. Schmit / J. W. Anderson / F. C. Vote | AIAA | 1981

    An Evaluation of Ablation Mechanisms for the Apollo Heat Shield Material

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

    SYNOPTIC : Orbit and Position Determination for Mars Orbiters and Landers

    R. H. Tolson / W T. Blackshear / S. G. Anderson | AIAA | 1970

    Estimating the Low-Speed Downwash Angle on an Aft Tail

    W. F. Phillips / E. A. Anderson / J. C. Jenkins et al. | AIAA | 2002

    Design and fabrication techniques for a large titanium 15-3-3-3 propellant tank

    KNAUER, C. D. / ANDERSON, F. W. / EDMAN, R. | AIAA | 1993

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

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

    Annular Suspension and Pointing System

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

    Advanced mass memories

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

    Improvement of normalization methods for eigenvector derivatives

    ELDRED, M. S. / LERNER, P. B. / ANDERSON, W. J. | AIAA | 1992