61–80 von 232 Ergebnissen
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    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

    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