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Search without synonyms: title: 23rd Aerospace Sciences Meeting

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    3D-Euler calculations using characteristic flux extrapolation

    EBERLE, A. | AIAA | 1985

    2011 Mars Science Laboratory Trajectory Reconstruction and Performance From Launch Through Landing (AAS 13-234)

    Abilleira, F. / American Astronautical Society / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2013

    Abort Options for Human Missions to Earth-Moon Halo Orbits (AAS 13-341)

    Jesick, M. / American Astronautical Society / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2013

    A Catalogue-Wide Implementation of General Perturbations Orbit Determination Extrapolated From Higher Order Orbital Theory Solutions (AAS 13-240)

    Hejduk, M.D. / Casali, S.J. / Cappellucci, D.A. et al. | British Library Conference Proceedings | 2013

    Accelerated convergence for incompressible flow calculations

    NEELY, G. / CLAUS, R. | AIAA | 1985

    Accurate and Fast Orbit Propagation With a New Complete Set of Elements (AAS 13-491)

    Bau, G. / Bombardelli, C. / Pelaez, J. et al. | British Library Conference Proceedings | 2013

    A class of airfoils having finite trailing edge pressure gradients

    ORMSBEE, A. / MAUGHMER, M. | AIAA | 1985

    A comparative study between an implicit and explicit algorithm for transonic airfoils

    VISBAL, M. / SHANG, J. | AIAA | 1985

    A comparison between theoretical and experimental flow fields of an airfoil with deflected spoiler

    LEE, C. / BODAPATI, S. | AIAA | 1985

    A comparison of Euler and Navier-Stokes solutions for supersonic flow over a conical delta wing

    NEWSOME, R. | AIAA | 1985

    A comparison of flight test and analytical techniques for boundary layer transition on a sailplane

    MILLER, K. | AIAA | 1985

    A computational method for determining detonation cell size

    KAILASANATH, K. / ORAN, E. / BORIS, J. et al. | AIAA | 1985

    A computational study of saddle point separation and horseshoe vortex system

    KAUL, U. / KWAK, D. / WAGNER, C. | AIAA | 1985

    A consideration of atomic oxygen interactions with space station

    LEGER, L. / VISENTINE, J. / SCHLIESING, J. | AIAA | 1985

    Adaptive torque equilibrium control of the Space Station

    SHAIN, E. / SPECTOR, V. | AIAA | 1985

    Aerodynamic configured missiles - Promise and future

    KRIEGER, R. | AIAA | 1985

    Aerodynamic effects of probe-induced flow separation of bluff bodiesat transonic Mach numbers

    HAUPT, B. / BUFF, R. / KOENIG, K. | AIAA | 1985

    Aerodynamic prediction of eliptically-shaped missile configurations using component build-up methodology

    VUKELICH, S. | AIAA | 1985

    Aerodynamics of an airfoil in ground effect with a jet issuing from its undersurface

    AGARWAL, R. / DEESE, J. | AIAA | 1985

    Aerodynamics of an aspect ratio 8 wing at low Reynolds numbers

    MARCHMAN, III, J. | AIAA | 1985

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