1–20 of 93 hits
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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

    Hot-shot gas source for pulsed MHD ACCELERATOR.

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

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

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

    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

    Evaluation of Fluid Behavior in Spinning Toroidal Tanks

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

    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

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

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

    Model and full-scale large transport airframe noise

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

    Feasibility Study of Developing Torodial Tanks for a Spinning Spacecraft

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

    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

    Mechanism of Combustion Instability in a Lean Premixed Dump Combustor

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

    Numerical prediction of turbulent flow over surface-mounted ribs

    BENODEKAR, R. W. / GODDARD, A. J. H. / GOSMAN, A. D. et al. | AIAA | 1985

    Improved Aerodynamic-Ramp Injector in Supersonic Flow

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

    Measurements of solid particles rebound characteristics on cylindrical targets

    Tabakoff, W. / Gunaraj, J. / Hamed, A. et al. | AIAA | 1996

    Integration of an Aeroramp Injector/Plasma Igniter for Hydrocarbon Scramjets

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