1–20 of 103 hits
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    Whither reliabilityques

    DE S. COUTINHO / J. | AIAA | 1965

    Synthesis of structural damping.

    BIEBER, R. E. | AIAA | 1968

    Local flow effects on base pressure.

    CASSANTO, J. M. | AIAA | 1968

    Aerodynamic characteristics for a slender missile with wrap-around fins

    CATANI, U. / DE AMICIS / R. et al. | AIAA | 1983

    Large space observatories of the 21st century

    NEIN, M. / HOWELL, J. / MORGAN, S. et al. | AIAA | 1987

    Development and pre-flight testing of the Olympus propulsion subsystem

    DEVEY, R. / GAYDON, S. / STATHAM, G. et al. | AIAA | 1989

    Liquid atomization by coaxial rocket injectors

    SANKAR, S. / BRENA DE LA ROSA, A / ISAKOVIC, A. et al. | AIAA | 1991

    Calculation of the two-phase aft-dome flowfield in solid rocket motors

    MADABHUSHI, RAVI K. / SABNIS, JAYANT S. / DE JONG et al. | AIAA | 1991

    Hybrid Navier-Stokes/Monte Carlo method for reacting flow calculations

    DE JONG / FREDERIK J. / SABNIS, JAYANT S. et al. | AIAA | 1992

    Characterization of coaxial rocket injector sprays under high pressure environments

    SANKAR, S. / WANG, G. / BRENA DE LA ROSA, A. et al. | AIAA | 1992

    Calculation of particle trajectories in solid-rocket motors with arbitrary acceleration

    SABNIS, JAYANT S. / DE JONG / FREDERICK J. et al. | AIAA | 1992