1–20 von 147 Ergebnissen
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    2001 Mars Odyssey Orbit Determination During Interplanetary Cruise

    P. G. Antreasian / D. T. Baird / J. S. Border et al. | AIAA | 2005

    A comprehensive model for AP-based composite propellant ignition

    KUMAR, M. / WILLS, J. E. / KULKARNI, A. K. et al. | AIAA | 1984

    Acoustic-vortex interactions and low-frequency oscillations in axisymmetric combustors

    KAILASANATH, K. / GARDNER, J. H. / BORIS, J. P. et al. | AIAA | 1989

    Aeroacoustic Characterization of Single- and Multiscale Porous Fences

    Rodríguez-López, Eduardo / Brizzi, Laurent E. / Valeau, Vincent et al. | AIAA | 2017

    Aerodynamic side force induced by nozzle entrance flow asymmetry

    VARWIG, R. L. / WHITTIER, J. S. / DURRAN, D. A. et al. | AIAA | 1989

    Aeroelastic design optimization program

    DODD, A. J. / KADRINKA, K. E. / LOIKKANEN, M. J. et al. | AIAA | 1990

    A Laser System to Measure Rocket Attitude in Flight

    K. M. Pell / J. E. Nydahl / R. G. Conard et al. | AIAA | 1978

    An existing facility for scramjet testing - The wave superheater.

    CARPENTER, J. E. / GRAVES, K. W. | AIAA | 1967

    Application of Encke's method to long arc orbit determination solutions

    LUNDBERG, J. B. / SCHUTZ, B. E. / FIELDS, R. K. et al. | AIAA | 1991

    A Relaxation Solution of Transonic Nozzle Flows Including Rotational Flow Effects

    E. F. Brown / T. J. F. Brechtt / K. E. Walsh | AIAA | 1977

    Assessment of Computational Fluid Dynamics for Supersonic Shock Containing Jets

    Miller, Steven A. E. / Veltin, Jérémy / Morris, Philip J. et al. | AIAA | 2009

    Boundary-layer development on moving walls using an integral theory

    FANSLER, K. S. / DANBERG, J. E. | AIAA | 1976

    Boundary-layer separation on moving walls using an integral theory

    FANSLER, K. S. / DANBERG, J. E. | AIAA | 1977