1–50 von 71 Ergebnissen
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    V/STOL demonstrator vehicle for ejector thrust augmentation technology

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

    Viscous shock-layer analysis of hypersonic flows over long slender bodies

    GUPTA, R. / LEE, K. / MOSS, J. et al. | AIAA | 1987

    Venus Geoscience Aerobot Study (VEGAS)

    Bachelder, A. / Nock, K. / Heun, M. et al. | AIAA | 1999

    Unsteady motion induced on a flexible surface in a high Reynolds number flow

    Anantha, K. / Varley, E. / Walker, J. | AIAA | 1996

    Turbulent viscous-shock-layer solutions with strong vorticity interaction

    ANDERSON, E. / MOSS, J. / SUTTON, K. | AIAA | 1976

    Treatment of source terms and high aspect ratio meshes in turbulence modelling

    Merci, B. / Steelant, J. / Vierendeels, J. et al. | AIAA | 1999

    Total pressure loss in vortical solutions of the conical Euler equations

    POWELL, K. / MURMAN, E. / PEREZ, E. et al. | AIAA | 1985

    The development of a Planetary Aerobot Testbed

    Nock, K. / Anderson, J. / Bachelder, A. et al. | AIAA | 1997

    Testing of an advanced liquid hydrogen turbopump

    Grabowski, R. / Chapman, L. / Crease, G. et al. | AIAA | 2000

    Supersonic dynamic stability experiments on the space shuttle

    ORLIK-RUECKEMANN, K. / LABERGE, J. / HANFF, E. | AIAA | 1972

    Solar simulation testing of the nuclear test detection spacecraft

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

    Smart fuels - 'Controlled' chemically reacting

    Maurice, L. / Corporan, E. / Minus, D. et al. | AIAA | 1999

    Self organization in 2D circular shear layers

    Coutsias, E. / Bergeron, K. / Lynov, J. et al. | AIAA | 1994

    Return to the Flight of M-V Rocket

    Onoda, J. / Sato, E. / Inatani, Y. et al. | AIAA | 2004

    Recession behavior of graphitic nozzles in simulated rocket motors

    KESWANI, S. / ANDIROGLU, E. / CAMPBELL, J. et al. | AIAA | 1983

    Radiatively driven wind tunnel experiment with a 30 kW electron beam

    Barker, P. / Grinstead, J. / Morgan, A. et al. | AIAA | 1999

    Prediction of unstart phenomena in hypersonic aircraft

    Cox, C / Lewis, C / Pap, R et al. | AIAA | 1995

    Performance of a Low Density Ablative Heat Shield Material

    Covington, M. A. / Balboni, J. A. / Chen, Y-K et al. | AIAA | 2004

    Passive control of flow separation over delta wings at high angle-of-attack

    Van Dyken, R. / Yu, K. / Gutmark, E. et al. | AIAA | 1996

    Orbital parameters for objects observed by the Mic...

    Abercromby, K. J. / Seitzer, P. / Parr-Thumm, T. L. et al. | AIAA | 2005

    Optical measurements of the orbital debris environment

    Jarvis, K. / Africano, J. / Stansbery, E. | AIAA | 2000

    Optically pumped and controlled electric discharges

    Macheret, Sergey / Barker, P. / Miles, Richard et al. | AIAA | 1999

    Oblique detonation wave studies in the Caltech T-5 Shock Tunnel Facility

    Sterling, J. / Cummings, E. / Ghorbanian, K. et al. | AIAA | 1998

    Numerical simulations of transient flows in ram accelerators

    LI, CHIPING / KAILASANATH, K. / ORAN, E. et al. | AIAA | 1993

    Numerical simulations of the reactive flow field in an axisymmetric combustor

    KAILASANATH, K. / GARDNER, J. / ORAN, E. et al. | AIAA | 1987

    Numerical simulations of high-speed flows in an axisymmetric ramjet

    KAILASANATH, K. / GARDNER, J. / ORAN, E. et al. | AIAA | 1988

    Numerical simulations of flow modification of supersonic rectangular jets

    Kolbe, R / Kailasanath, K / Young, T et al. | AIAA | 1995

    New concept of small satellite, HETE-2 and its sci...

    Matsuoka, M. / Kawai, N. / Yoshida, A. et al. | AIAA | 2005

    Monolithic Fuel Cells

    Fee, D. C. / Billone, M. C. / Busch, D. E. et al. | AIAA | 1987

    Measurement of dynamic cross-derivatives due to pitching and yawing

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

    Mars Exploration Deep Space Return Link Scenarios ...

    Noreen, Gary K. / Williams, W. Dan / Sands, O. Scott et al. | AIAA | 2005

    Line relaxation methods for the solution of 2D and 3D compressible flows

    HASSAN, O. / PROBERT, E. / MORGAN, K. et al. | AIAA | 1993

    Laser and radiofrequency production of seeded air plasmas

    Scharer, J. / Ding, G. / Gui, H. et al. | AIAA | 1999

    Laminar boundary layer stability experiments on a cone at Mach 8. I - Sharp cone

    STETSON, K. / THOMPSON, E. / DONALDSON, J. et al. | AIAA | 1983

    IVHM (Integrated Vehicle Health Management) techniques for future space vehicles

    Baroth, E. / Powers, W. / Fox, J. et al. | AIAA | 2001

    Introducing the ESA DRAMA Tool

    Martin, C. E. / Cheese, J. E. / Sánchez-Ortiz, N. et al. | AIAA | 2004

    Interactions between acoustics and vortex structures in a central dump combustor

    KAILASANATH, K. / GARDNER, J. / BORIS, J. et al. | AIAA | 1986

    Initial radiation measurement results from Europe's Galileo test-bed satellite, Giove-A

    Ryden, K. A. / Morris, P. A. / Rodgers, D. J et al. | AIAA | 2006

    Improvement of disk MHD generator performance by inlet swirl

    Yamasaki, H. / Okuno, Y. / Torii, S. et al. | AIAA | 1999

    Heat pipe avionic thermal control

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

    Effects of energy release on high-speed flows in an axisymmetric combustor

    KAILASANATH, K. / GARDNER, J. / ORAN, E. et al. | AIAA | 1989

    Downstream mixing gasdynamic lasers - A numerical solution

    PARTHASARATHY, K. / ANDERSON, JR., J. / JONES, E. | AIAA | 1979

    Design and performance evaluation of a two-position variable geometry turbofan combustor

    SANBORN, J. / SCHEIHING, P. / COLEMAN, E. et al. | AIAA | 1984