1–20 von 93 Ergebnissen
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    Time-marching transonic flutter solutions including angle-of-attack effects

    EDWARDS, J. W. / BENNETT, R. M. / WHITLOW, W. et al. | AIAA | 1983

    Ignition of ammonium perchlorate composite propellants by convectiveheating.

    BAER, A. D. / KELLER, J. A. / RYAN, N. W. | AIAA | 1966

    Efficiency of a Constant-Area, Adiabatic Tip, Heat Pipe Fin

    W. J. Bowman / T. W. Moss / D. Maynes et al. | AIAA | 2000

    Hot-shot gas source for pulsed MHD ACCELERATOR.

    DURRAN, D. A. / GRABOWSKY, W. R. / SPENCER, D. J. | AIAA | 1967

    Two-stream, supersonic, wake flowfield behind a thick base. I - General features

    AMATUCCI, V. A. / DUTTON, J. C. / KUNTZ, D. W. et al. | AIAA | 1992

    Feasibility Study of Developing Torodial Tanks for a Spinning Spacecraft

    J. E. Anderson / D. A. Fester / D. W. Dugan | AIAA | 1975

    Model and full-scale large transport airframe noise

    SHEARIN, J. / FRATELLO, D. / BOHN, A. et al. | AIAA | 1976

    Evaluation of Fluid Behavior in Spinning Toroidal Tanks

    J. E. Anderson / D. A. Fester / D. W. Dugan | AIAA | 1977

    Influence of Curvature-Driven Favorable Pressure Gradient on Supersonic Turbulent Boundary Layer

    Joel J. Luker / Rodney D. W. Bowersox / Thomas A. Buter | AIAA | 2000

    Numerical simulation of tip vortices of wings in subsonic and transonic flows

    SRINASAN, G. R. / MCCROSKEY, W. J. / BAEDER, J. D. et al. | AIAA | 1988

    A study of fog clearing using a CO2 laser

    CHRISTIANSEN, W. H. / MULLANEY, G. J. / RUSSELL, D. A. | AIAA | 1971

    Mechanism of Combustion Instability in a Lean Premixed Dump Combustor

    K. K. Venkataraman / L. H. Preston / D. W. Simons et al. | AIAA | 1999

    Experiments using a 25-kw hollow cathode lithium vapor MPD arcjet

    BLACKSTOCK, A. W. / FRADKIN, D. B. / LIEWER, K. W. et al. | AIAA | 1970

    Chemical and nozzle flow losses in hypersonic ramjets

    BLACKMAN, A. W. / MIGDAL, D. / SARLI, V. J. | AIAA | 1965

    Optimization of Orifice Geometry for Crossflow Mixing in a Cylindrical Duct

    J. T. Kroll / W. A. Sowa / G. S. Samuelsen et al. | AIAA | 2000

    Improved Aerodynamic-Ramp Injector in Supersonic Flow

    L. S. Jacobsen / S. D. Gallimore / J. A. Schetz et al. | AIAA | 2003

    Progress report on the engineering development of the Magnus Aerospace LTA 20-1 airship

    DELAURIER, J. / MCKINNEY, W. / LOWE, J. et al. | AIAA | 1985

    Application of multivariable linear control design to marine towed systems

    Kamman, J. W. / Patek, S. D. / Hoeckley, S. A. | AIAA | 1996