1–20 of 131 hits
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    Multiple element airfoils optimized for maximum lift coefficient.

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

    The mechanical and thermal properties of CU-infiltrated P/M tungstennozzles

    HSU, S.-E. / CHEN, C.-I. / SHEN, Y. et al. | AIAA | 1976

    Transonic Computational Analysis of F-111 TACT

    A. W. Chen / E. N. Tinocot / H. Yoshihara | AIAA | 1978

    New Approach to the 3-D Transonic Flow Analysis Using the STAR-106 Computer

    David D. Redhed / Allen W. Chen / Steven G. Hotovy | AIAA | 1979

    Postbuckling behavior of a thick plate

    CHEN, L.-W. / DOONG, J.-L. | AIAA | 1983

    PAN AIR applications to aero-propulsion integration

    CHEN, A. W. / TINOCO, E. N. | AIAA | 1984

    Reply by Authors to W.C. Chin

    Allen W Chen / Edward N Tinow | AIAA | 1984

    Dynamic ground effects on a two-dimensional flat plate

    CHEN, Y.-S. / SCHWEIKHARD, W. G. | AIAA | 1985

    Computational method for optimization of structural shapes

    HOU, J. W. / CHEN, J. L. / SHEEN,J. S. | AIAA | 1986

    Autonomous spin axis controller for geostationary spinning satellites

    CHEN, C. / SLAFER, L. / HUMMEL, JR., W. | AIAA | 1986