151–200 von 232 Ergebnissen
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    Comet plasma tail formation — Giotto observations

    Wilken, B. / Jockers, K. / Johnstone, A.D. et al. | Elsevier | 1986

    Total pressure loss in vortical solutions of the conical Euler equations

    POWELL, K. / MURMAN, E. / PEREZ, E. et al. | AIAA | 1985

    Recession behavior of graphitic nozzles in simulated rocket motors

    KESWANI, S. T. / ANDIROGLU, E. / CAMPBELL, J. D. et al. | AIAA | 1985

    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

    Classical and neo-classical cruise-dash optimization

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

    Experimental aerodynamic characteristics of an NACA 0012 airfoil with simulated ice

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

    Generalized math model for simulation of high-altitude balloon systems

    NIGRO, N. J. / ELKOUH, A. F. / HINTON, D. E. et al. | AIAA | 1985

    Comet Halley: Nucleus and jets (results of the VEGA mission)

    Sagdeev, R.Z. / Avanesov, G.A. / Barinov, I.V. et al. | Elsevier | 1985

    Maximum loading capability of axial flow compressors

    SCHWEITZER, J. K. / GARBEROGLIO, J. E. | AIAA | 1984

    Energy Dissipation Due to Vehicle/Track Interaction

    Dzielski, J. E. / Hedrick, J. K. | Taylor & Francis Verlag | 1984

    A comprehensive model for AP-based composite propellant ignition

    KUMAR, M. / WILLS, J. E. / KULKARNI, A. K. et al. | AIAA | 1984

    Performance degradation of a model helicopter rotor with a generic ice shape

    KORKAN, K. D. / CROSS, E. J. / MILLER, T. L. | AIAA | 1984

    Space Shuttle contamination measurements from flights STS-1 through STS-4

    EHLERS, H. K. F. / JACOBS, S. / LEGER, L. J. et al. | AIAA | 1984

    Design and performance evaluation of a two-position variable geometry turbofan combustor

    SANBORN, J. / SCHEIHING, P. / COLEMAN, E. et al. | AIAA | 1984

    Performance of differenced range data types in Voyager navigation

    TAYLOR, T. H. / CAMPBELL, J. K. / JACOBSON, R. A. et al. | AIAA | 1984

    Laminar boundary layer stability experiments on a cone at Mach 8. I - Sharp cone

    STETSON, K. / THOMPSON, E. / DONALDSON, J. et al. | AIAA | 1983

    Nonlinear inverse perturbation method in dynamic analysis

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

    Recession behavior of graphitic nozzles in simulated rocket motors

    KESWANI, S. / ANDIROGLU, E. / CAMPBELL, J. et al. | AIAA | 1983

    Simple model for base pressure effects in source flow chemical lasers

    PATTERSON, K. E. / BATTEH, J. H. / HOWIE, S. S. | AIAA | 1983

    Model for pure source flow chemical lasers

    PATTERSON, K. E. / BATTEH, J. H. / HOWIE, S. S. | AIAA | 1983

    Forced Steering of Rail Vehicles: Stability and Curving Mechanics

    BELL, C. E. / HEDRICK, J. K. | Taylor & Francis Verlag | 1981

    Combustion of ammonium perchlorate-polymer sandwiches

    PRICE, E. W. / HANDLEY, J. C. / PANYAM, R. R. et al. | AIAA | 1981

    Heat pipe avionic thermal control

    TOKEN, K. / GARNER, E. / COOK, R. et al. | AIAA | 1980

    Transport Property Correlations for H2-He Gas Mixtures at Temperatures of 1000-25,000

    K E. V. Zoby / R. A. Graves J. N. Moss / T A. Kumar et al. | AIAA | 1980

    Approximate convective heating equations for hypersonic flows

    ZOBY, E. / MOSS, J. / SUTTON, K. | AIAA | 1979

    Downstream mixing gasdynamic lasers - A numerical solution

    PARTHASARATHY, K. / ANDERSON, JR., J. / JONES, E. | AIAA | 1979

    Downstream Mixing Gasdynamic Lasers-A Numerical Solution

    K. N. ParthaSarathy / J. D. Anderson E. Jones | AIAA | 1979

    Wind-Tunnel Measurement of Dynamic Cross-Coupling Derivatives

    E. S. Hanff / K. J. Orlik-Ruckemann | AIAA | 1978

    Application of skin technology to turbine blades

    WORTMANN, J. / SCHWEITZER, K. / SPRENGER, H. et al. | AIAA | 1978

    A Laser System to Measure Rocket Attitude in Flight

    K. M. Pell / J. E. Nydahl / R. G. Conard et al. | AIAA | 1978

    Boundary-layer separation on moving walls using an integral theory

    FANSLER, K. S. / DANBERG, J. E. | AIAA | 1977

    A Relaxation Solution of Transonic Nozzle Flows Including Rotational Flow Effects

    E. F. Brown / T. J. F. Brechtt / K. E. Walsh | AIAA | 1977

    Turbulent viscous-shock-layer solutions with strong vorticity interaction

    ANDERSON, E. / MOSS, J. / SUTTON, K. | AIAA | 1976

    Boundary-layer development on moving walls using an integral theory

    FANSLER, K. S. / DANBERG, J. E. | AIAA | 1976

    Mechanisms of transonic blade-vortex interaction noise

    LENT, H.-M. / MEIER, G. E. A. / MUELLER, K. J. et al. | AIAA | 1976