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    3-D finite element solution of steady Euler transonic flow by streamvector correction

    EL DABAGHI, F. / PIRONNEAU, O. / PERIAUX, J. et al. | AIAA | 1985

    3-D LDV measurements over a delta wing in pitch-up motion

    HOANG, N. / REDINIOTIS, O. / TELIONIS, D. | AIAA | 1993

    A Bayesian analysis of the “accident rate potential” parameter

    Williford, William O. / Barton, Henry E. | Elsevier | 1974

    Ablation of Leonid meteoroids

    Popova, O. | AIAA | 2000

    Abort capabilities of rocket-powered single-stage launch vehicles

    STANLEY, DOUGLAS O. / POWELL, RICHARD W. | AIAA | 1991

    About some aspects of the creation of the solar engine with post-burning

    Kudrin, O / Nikoenko, V / Finogenov, S | AIAA | 1995

    Accessibility of near-earth asteroids

    LAU, C. O. / HULKOWER, N. D. | AIAA | 1987

    Accurate and efficient vortex-capturing for rotor blade-vortex interaction

    Boelens, O. / van der Ven, H. / Oskam, B. et al. | AIAA | 2000

    A collaborative numerical and experimental investigation of flapping-wing propulsion

    Jones, K. / Castro, B. / Mahmoud, O. et al. | AIAA | 2002

    A comparison of four viscous models for the discrete vortex method

    Takeda, K. / Tutty, O. / Fitt, A. | AIAA | 1997