121–140 von 236 Ergebnissen
|

    Radiation exchange in large space structure and frames

    EMERY, A. F. / MORTAZAVI, H. R. / NGUYEN, M. N. | AIAA | 1985

    Thrust Imbalance of the Space Shuttle Solid Rocket Motors

    Winfred A. Foster m Richard H. Sforzini / Benjamin W. Shackelford | AIAA | 1982

    Roll-up of aircraft trailing vortices using artificial viscosity

    BLOOM, A. M. / George Washington University / Washington et al. | AIAA | 1974

    Symmetric body vortices on slender bodies of revolution at transonicspeeds

    DEANE, J. R. / PONTING, M. H. / FELLOWS, K. A. | AIAA | 1980

    Investigation of unsteady subsonic spoiler and flap aerodynamics

    COSTES, M. / GRAVELLE, A. / PHILIPPE, J. J. et al. | AIAA | 1987

    Inlet Design Studies for a Mach 2.2 Advanced Supersonic Cruise Vehicle

    K. M. Shimabukuro / H. R. Welge / A. C. Lee | AIAA | 1982

    Polymer pyrolysis over a wide range of heating rates

    BAER, A. D. / HEDGES, J. H. / SEADER, J. D. et al. | AIAA | 1977

    New formulation for one-dimensional premixed flames

    MUKUNDA, H. S. / DESHPANDE, S. M. / BHASHYAM, A. T. | AIAA | 1986

    Design for the future in terminal air traffic control.

    BURNS, H. C. / HOOTON, E. N. / WARSKOW, M. A. | AIAA | 1969

    Overview of the Development of Hydrazinium Nitroformate

    H. F. R. Sch-ograve / yer / W. H. M. Welland-Veltman et al. | AIAA | 2002

    Bow shock/jet interaction in compressible transverse injection flowfields

    Gruber, M. R. / Nejad, A. S. / Chen, T. H. et al. | AIAA | 1996

    A new approach to durability prediction for fuel tank skins

    FERMAN, M. A. / UNGER, W. H. / SAFF, C. R. et al. | AIAA | 1986

    Wing effects on missile asymmetric vortex behavior

    Howard, R. M. / Lung, M. H. / Viniotis, J. J. et al. | AIAA | 1994

    Temperature variation of the elastic constants of aluminum alloy 2090-T81

    MORRIS, J. W. / KIM, S. A. / AUSTIN, M. W. et al. | AIAA | 1987

    Pressure-Sensitive Paint Measurements on a Supersonic High-Sweep Oblique Wing Model

    B. G. McLachlan / J. H. Bell / H. Park et al. | AIAA | 1995

    Analysis of the argon additive influence on a nitrogen arcjet flow

    Schoenemann, A. T. / Auweter-Kurtz, M. / Habiger, H. A. et al. | AIAA | 1994

    High-performance propellants based on hydrazinium nitroformate

    Schoeyer, H. F. R. / Schnorhk, A. J. / Korting, P. A. O. G. et al. | AIAA | 1995