1–50 von 232 Ergebnissen
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    NONGRAY ERROR IN TOTAL EMITTANCE MEASUREMENTS

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

    Solar simulation testing of the nuclear test detection spacecraft

    GLENN, E. / GOLDMAN, K. / LEHR, S. et al. | AIAA | 1964

    A study of heterogeneous detonations

    RAGLAND, K. / DABORA, E. / NICHOLLS, J. | AIAA | 1966

    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

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

    Book reviews

    Rogers, K. G. / Weaver, T. E. / Maher, M. et al. | Taylor & Francis Verlag | 1972

    Inter‐urban roads in Great Britain: perspectives and prospects

    Judge, E. J. / Button, K. J. | Taylor & Francis Verlag | 1974

    Measurement of dynamic cross-derivatives due to pitching and yawing

    ORLIK-RUECKEMANN, K. / LABERGE, J. / HANFF, E. | AIAA | 1974

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

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

    V/STOL demonstrator vehicle for ejector thrust augmentation technology

    BYRNES, J. / MURPHY, R. / BALL, R. et al. | AIAA | 1974

    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

    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

    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

    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

    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

    Heat pipe avionic thermal control

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