1–20 of 207 hits
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    Finite difference scheme for automatic costate calculation

    Seywald, Hans / NASA, Langley Research Center / Hampton, VA et al. | AIAA | 1996

    Mixing of swirling jets in a supersonic duct flow

    Kraus, D. K. / NASA, Langley Research Center / Hampton, VA et al. | AIAA | 1996

    The supersonic transport : a technical summary

    Langley Research Center, Hampton, Va. | TIBKAT | 1960

    Free vibrations of multilayered composite plates.

    NOOR, A. K. / NASA, Langley Research Center / Hampton, Va. | AIAA | 1973

    Terminal Configurated Vehicle Program : test facilities guide

    Langley Research Center, Hampton, Va. | TIBKAT | 1980

    Effect of initial condition on subsonic jet noise

    ZAMAN, K. B. M. Q. / George Washington / University et al. | AIAA | 1985

    Long flight-time range-optimal aircraft trajectories

    Seywald, Hans / NASA, Langley Research Center / Hampton, VA | AIAA | 1996

    Radical wings & wind tunnels : advanced concepts tested at the NASA Langley

    Chambers, Joseph R. / Chambers, Mark A. / Langley Research Center, Hampton, Va. | TIBKAT | 2008

    Development of transonic area-rule methodology

    Carlsen, Wayne D. / NASA, Langley Research Center / Hampton, VA | AIAA | 1995

    Flow establishment in a generic scramjet combustor

    JACOBS, P. A. / NASA, Langley Research Center / Hampton, VA et al. | AIAA | 1992

    Hypersonic incipient separation on delta wing with trailing-edge flap

    RAO, D. M. / NASA, Langley Research Center / Hampton, Va. | AIAA | 1975

    Position accuracy of aircraft area navigation systems and the effectof system parameters

    FOUDRIAT, E. C. / NASA, Langley Research Center / Hampton, Va. | AIAA | 1975

    Nonlinear analysis of a cantilever beam

    HINNANT, HOWARD E. / NASA, Langley Research Center / Hampton, VA et al. | AIAA | 1988

    Multiple element airfoils optimized for maximum lift coefficient.

    ORMSBEE, A. I. / CHEN, A. W. / NASA, Langley Research Center et al. | AIAA | 1972