1–20 von 44 Ergebnissen
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    Active-Control System for Breakup of Airplane Trailing Vortices

    J. D. Crouch / G. D. Miller / P. R. Spalart | AIAA | 2001

    Leeside flows over delta wings at supersonic speeds

    MILLER, D. S. / WOOD, R. M. | AIAA | 1984

    Generalized Characteristics of Communication, Sensing, and Navigation Satellite Systems

    Graeme B. Shaw / D. W. Miller / D. E. Hastings | AIAA | 2000

    Evaluation of the Dynamic Environment of an Asteroid: Applications to 433 Eros

    D. J. Scheeres / B. G. Williams / J. K. Miller | AIAA | 2000

    Criteria for electrically heated temperature probes in flames.

    MILLER, I. M. / SCHRYER, D. R. | AIAA | 1972

    Summary of an Active Flexible Wing program

    Perry, Boyd / Cole, Stanley R. / Miller, Gerald D. | AIAA | 1995

    Research on vtol aircraft handling qualities criteria

    CLARK, J. W. / MILLER, D. P. | AIAA | 1965

    Computations of supersonic flows over a body at high angles of attack

    BAYSAL, O. / FOULADI, K. / MILLER, D. S. | AIAA | 1989

    Application of Finite-Element Theory to Airplane Configurations

    R. G. BRADLEY* AND B. D. MILLER | AIAA | 1971