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person:("Miller, D.")

    The stability of an elliptic jet

    MILLER, D. | AIAA | 1984

    Design study results of a supersonic cruise fighter wing

    MILLER, D. / SCHEMENSKY, R. | AIAA | 1979

    Leeside flows over delta wings at supersonic speeds

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

    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

    Trajectory design for a visible geosynchronous earth imager

    Kong, Edmund / Sedwick, R. / Miller, D. | AIAA | 1999

    An overview of two nonlinear supersonic wing design studies

    MILLER, D. / PITTMAN, J. / WOOD, R. | AIAA | 1983

    A supersonic maneuver wing designed for nonlinear attached flow

    MASON, W. / SICLARI, M. / MILLER, D. et al. | AIAA | 1983

    Deployable Inspector Spacecraft for Distributed Field Measurements

    Macke, Jared / Miller, D. / Swartwout, Michael et al. | AIAA | 2004

    Status review of a supersonically-biased fighter wing-design study

    WOOD, R. / MILLER, D. / HAHNE, D. et al. | AIAA | 1983

    Status review of a supersonically biased fighter wing design study

    WOOD, R. M. / MILLER, D. S. / HAHNE, D. E. et al. | AIAA | 1984

    Generalized Characteristics of Communication, Sensing, and Navigation Satellite Systems

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

    Mach 8 to 22 studies of flow separations due to deflected control surfaces

    CHILDS, M. E. / WASHINGTON, U. / DEPT. OF MECHANICAL ENGINEERING et al. | AIAA | 1964