1–50 von 481 Ergebnissen
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    Use of helium gas to reduce acoustic transmission

    BLEVINS, J. / HANSEN, L. | AIAA | 1985

    FINITE ELEMENT ANALYSIS OF THE IMPACT RESPONSE OF COMPOSITE PLATES AND SHELLS

    MONTEMURRO, M. / HANSEN, J. / HOUDE, M. | AIAA | 1993

    A global Navier-Stokes rotor prediction model

    Hansen, M. / Sorensen, J. / Michelsen, J. et al. | AIAA | 1997

    New approach to tracking engine life

    Suarez, E. / Hansen, J. / Duffy, M. et al. | AIAA | 1997

    Crashworthiness of aircraft fuselage structures

    TENNYSON, R. / HANSEN, J. / TEICHMAN, H. et al. | AIAA | 1978

    Missile aerodynamics prediction code

    SUN, J. / HANSEN, S. G. / CUMMINGS, R. M. et al. | AIAA | 1985

    Experimental Study of Near-Field Flow Structure in Hollow Cone Pressure Swirl Sprays

    J. L. Santolaya / L. A. Aísa / E. Calvo et al. | AIAA | 2007

    Calculations of the dilution system in an annular gas turbine combustor

    MCGUIRK, J. J. / PALMA, J. M. L. M. | AIAA | 1992

    Automatic formation flight control

    Pachter, M. / D'Azzo, J. J. / Dargan, J. L. | AIAA | 1994

    DRAG OF SPHERES IN RAREFIED HYPERVELOCITY FLOW

    KINSLOW, M. / POTTER, J. L. | AIAA | 1963

    Effects of GH/LOX Velocity and Momentum Ratios on Shear Coaxial Injector Atomization

    M. Ferraro / R. J. Kujala / J.-L. Thomas et al. | AIAA | 2002

    Circulation controlled STOL wing optimization

    LOTH, J. L. / BOASSON, M. | AIAA | 1984

    Propagation of Spinning Acoustic Modes in Turbofan Exhaust Ducts

    M. Nallasamy / D. L. Sutliff / L. J. Heidelberg | AIAA | 2000

    Large-Eddy-Simulation Modeling for Aerothermal Predictions Behind a Jet In Crossflow

    J. Jouhaud / L. Y. Gicquel / B. Enaux et al. | AIAA | 2007

    Viscous drag reduction using streamwise-aligned riblets

    VUKOSLAVCEVIC, P. / WALLACE, J. M. / BALINT, J.-L. | AIAA | 1992

    Optimizing distributed structures for maximum flutter load

    CLAUDON, J.-L. / SUNAKAWA, M. | AIAA | 1981

    Noninvasive experimental technique for the measurement of unsteady velocity fields

    LOURENCO, L. / KROTHAPALLI, A. / BUCHLIN, J. M. et al. | AIAA | 1986

    Large-Eddy Simulations and Lidar Measurements of Vortex-Pair Breakup in Aircraft Wakes

    D. C. Lewellen / W. S. Lewellen / L. R. Poole et al. | AIAA | 1998

    Bubble Bursting and Stall Hysteresis on Single-Slotted Flap High-Lift Configuration

    M. Baragona / L. M. M. Boermans / M. J. L. van Tooren et al. | AIAA | 2003

    Estimates of oxides of nitrogen formed in a scramjet inlet

    CHIAPPETTA, L. M. / SANGIOVANNI, J. J. | AIAA | 1991

    Nonlinear aerodynamic effects on bodies in supersonic flow

    PITTMAN, J. L. / SICLARI, M. J. | AIAA | 1984

    Nonequilibrium ionization due to electron heating - ii - experiments

    HOFFMAN, M. A. / KERREBROCK, J. L. | AIAA | 1964

    Low-Reynolds-number separation on an airfoil

    Lin, J. C. M. / Pauley, Laura L. | AIAA | 1996

    Influence of injectant Mach number and temperature on supersonic film cooling

    Juhany, K. A. / Hunt, M. L. / Sivo, J. M. | AIAA | 1994

    Liquid Rocket Engine Test Stand Planning

    Emdee, J. L. / Adams, M. J. / Rahman, S. | AIAA | 2005

    Automated control of aircraft in formation flight

    BUZOGANY, L. / PACHTER, M. / D'AZZO, J. | AIAA | 1993

    Radiative ignition of double base propellants. II - Pre-ignition events and source effects

    DELUCA, L. / OHLEMILLER, T. J. / CAVENY, L. H. et al. | AIAA | 1976

    Approximate optimal atmospheric entry trajectories.

    SPEYER, J. L. / WOMBLE, M. E. | AIAA | 1971

    Excitation of the Wall Region by Sound in Fully Developed Channel Flow

    K. M. M. Alshamani / J. L. Livesey / F. J. Edwards | AIAA | 1982

    Separated flow upstream of a jet in a crossflow

    KROTHAPALLI, A. / LOURENCO, L. / BUCHLIN, J. M. | AIAA | 1990

    Mission Analysis of Spinning Systems for Transfers from Low Orbits to Geostationary

    E. C. Lorenzini / M. L. Cosmo / M. Kaiser et al. | AIAA | 2000

    Random Packing of Heterogeneous Propellants

    G. M. Knott / T. L. Jackson / J. Buckmaster | AIAA | 2001

    Initial conditions for the hypersonic-shock/boundary-layer interaction problem.

    WERLE, M. J. / DWOYER, D. L. / HANKEY, W. L. | AIAA | 1973

    Wake Alleviation Properties of Triangular-Flapped Wings

    J. M. Ortega / R. L. Bristol / O. Savas | AIAA | 2002

    Verification tests of durable thermal protection system concepts

    SHIDELER, J. L. / WEBB, G. L. / PITTMAN, C. M. | AIAA | 1985

    Radiative ignition of double-base propellants. I - Some formulation effects

    DELUCA, L. / CAVENY, L. H. / OHLEMILLER, T. J. et al. | AIAA | 1976