1–50 von 151 Ergebnissen
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    NONGRAY ERROR IN TOTAL EMITTANCE MEASUREMENTS

    BEVANS, J. T. / NELSON, K. E. | AIAA | 1963

    Feasibility studies of a rotating detonation wave rocket motor.

    CULLEN, R. E. / NICHOLLS, J. A. / RAGLAND, K. W. | AIAA | 1966

    Solar simulation testing of the nuclear test detection spacecraft.

    GLENN, E. E. / GOLDMAN, K. L. / LEHR, S. N. et al. | AIAA | 1966

    An existing facility for scramjet testing - The wave superheater.

    CARPENTER, J. E. / GRAVES, K. W. | AIAA | 1967

    Pressure distribution on cone-cylinders in hypersonic flow.

    CLARK, G. E. / RIGALI, D. J. | AIAA | 1968

    Optimal estimation of rotation-coupled flexural oscillations

    FARRELL, J. L. / MILLER, J. A. / NEWTON, J. K. et al. | AIAA | 1969

    Orbit determination using analytic partial derivatives of perturbed motion

    ARSENAULT, J. L. / FORD, K. C. / KOSKELA, P. E. | AIAA | 1970

    Three-Dimensional^ Minimum Fuel Turns for a Supersonic Aircraft

    J. K. HEDRICK AND A. E. BRYSON / JR | AIAA | 1972

    Supersonic Dynamic Stability Experiments on the Space Shuttle

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

    Surface Flow Patterns and Aerodynamic Heating on Space Shuttle Vehicles

    J. G. MARVIN / H. L. SEEGMILLER / W. K. LOCKMAN et al. | AIAA | 1972

    Pitch Axis Stabilization in Eccentric Orbits Using a Variable-Speed Rotor

    R. E. LOHFELD / D. K. ANAND AND J. M. WHISNANT | AIAA | 1974

    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

    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

    Wind-Tunnel Measurement of Dynamic Cross-Coupling Derivatives

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

    A Laser System to Measure Rocket Attitude in Flight

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

    Downstream Mixing Gasdynamic Lasers-A Numerical Solution

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

    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

    Combustion of ammonium perchlorate-polymer sandwiches

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

    Nonlinear inverse perturbation method in dynamic analysis

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

    Maximum loading capability of axial flow compressors

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

    Performance of differenced range data types in Voyager navigation

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

    Recession behavior of graphitic nozzles in simulated rocket motors

    KESWANI, S. T. / ANDIROGLU, E. / CAMPBELL, J. D. 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