101–120 von 232 Ergebnissen
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    A computational method for determining detonation cell size

    KAILASANATH, K. / ORAN, E. / BORIS, J. et al. | AIAA | 1985

    Discontinuous wing leading edge to enhance spin resistance

    DICARLO, D. J. / GLOVER, K. E. / STEWART, E. C. et al. | AIAA | 1985

    Depriming/rewetting of arterial heat pipes - Comparison with Share-II flight experiment

    Ochterbeck, J. M. / Peterson, G. P. / Ungar, E. K. | AIAA | 1995

    Line relaxation methods for the solution of 2D and 3D compressible flows

    HASSAN, O. / PROBERT, E. / MORGAN, K. et al. | AIAA | 1993

    A new relative referencing method for crop monitoring using chlorophyll fluorescence

    Norikane, J. / Goto, E. / Kurata, K. et al. | Elsevier | 2002

    Classical and neo-classical cruise-dash optimization

    BILIMORIA, K. D. / CLIFF, E. M. / KELLEY, H. J. | AIAA | 1985

    Numerical evaluation of propeller noise including nonlinear effects

    KORKAN, K. D. / VON LAVANTE / E. et al. | AIAA | 1986

    Design and operation of a supersonic annular flow facility

    Williams, K. E. / Gessner, F. B. / Harloff, G. J. | AIAA | 1994

    Supersonic dynamic stability experiments on the space shuttle

    ORLIK-RUECKEMANN, K. / LABERGE, J. / HANFF, E. | AIAA | 1972

    Validation of an Experimentally Derived Uncertainty Model

    K. B. Lim / D. E. Cox / G. J. Balas et al. | AIAA | 1998

    The Application of Quasi-Linearization to the Prediction of Nonlinear Railway Vehicle Response

    COOPERRIDER, N. K. / HEDRICK, J. K. / LAW, E. H. et al. | Taylor & Francis Verlag | 1975

    Investigation of supersonic flow about strut/endwall intersections in an annular duct

    Williams, K. E. / Harloff, G. J. / Gessner, F. B. | AIAA | 1995

    Mixing and combustion in a spinning combustor

    WILSON, K. J. / SCHADOW, K. C. / GUTMARK, E. et al. | AIAA | 1992

    Supersonic Dynamic Stability Experiments on the Space Shuttle

    K. J. ORLIK-RUCKEMANN / J. G. LABERGE AND E. S. HANFF | AIAA | 1972

    Experimental aerodynamic characteristics of an NACA 0012 airfoil with simulated ice

    KORKAN, K. D. / CROSS, E. J. / CORNELL, C. C. | AIAA | 1985

    Compressive Response of Lightweight Ceramic Ablators: Phenolic Impregnated Carbon Ablator

    Kelly E. Parmenter / Karl Shuman / Frederick Milstein et al. | AIAA | 2001