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    Improved measurement of depth perception

    Fitch, R. C. / Miller, D. D. | NTRS | 1972

    RELIABILITY-MAINTAINABILITY COST TRADE-OFF VIA DYNAMIC AND LINEAR PROGRAMMING

    REICH, W. / FLANNERY, W. / MILLER, D. | AIAA | 1966

    Extended Bandwidth Instrument Pointing and S/C G&C - The Middeck Active Control Experiment (MACE)

    Miller, D. W. / How, J. P. | British Library Conference Proceedings | 1996

    Comparison of computations and experimental data for leading edge vortices - Effects of yaw and vortex flaps

    MURMAN, E. / POWELL, K. / MILLER, D. et al. | AIAA | 1986

    Launch Load Alleviation for Lightweight, Active Mirrors

    Cohan, L. / Miller, D. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2010

    Aerodynamic design considerations for efficient high-lift supersonic wings

    Miller, D. S. / Wood, R. M. | NTRS | 1986

    Influence of leading-edge thrust on twisted and cambered wing design for suersonic cruise

    Carlson, H. W. / Miller, D. S. | NTRS | 1983

    Experimental investigation of leading-edge thrust at supersonic speeds

    Wood, R. M. / Miller, D. S. | NTRS | 1983

    Performance verification of an air solar collector

    Miller, D. C. / Romaker, R. F. | NTRS | 1979

    Noise predictions and economic effects of Boeing nacelle modifications

    Miller, D. S. / Nordstrom, D. C. | NTRS | 1968

    Aerodynamic design considerations for efficient high-lift supersonicwings

    MILLER, D. S. / WOOD, R. M. | AIAA | 1986

    Fundamental aerodynamic characteristics of delta wings with leading-edge vortex flows

    Wood, R. M. / Miller, D. S. | NTRS | 1985

    An overview of two nonlinear supersonic wing design studies

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

      An overview of two nonlinear supersonic wing design studies

      Miller, D. S. / Pittman, J. L. / Wood, R. M. | NTRS | 1983

    A study of the application of heat or force fields to the sonic-boom-minimization problem

    Carlson, H. W. / Miller, D. S. | NTRS | 1969

    The polar platform of the Space Station - A permanent facility for meteorological, oceanographic, and land observations

    HEACOCK, E. / MILLER, D. / SCHNEIDER, S. | AIAA | 1986

    Assessment of preliminary prediction techniques for wing leading-edge vortex flows at supersonic speeds

    Wood, R. M. / Miller, D. S. | NTRS | 1985

    Wing planform effects at supersonic speeds for an advanced fighter configuration

    Wood, R. M. / Miller, D. S. | NTRS | 1984

    Leeside flows over delta wings at supersonic speeds

    Miller, D. S. / Wood, R. M. | NTRS | 1984

    Stimulus generalization of gravity produced by variations in angularvelocity and radius

    LOVE, C. / MCCOY, D. / MILLER, D. | AIAA | 1971

    Computations of vortical supersonic flows over a blunt-nose-cylinderat high angles of attack

    BAYSAL, O. / FOULADI, K. / MILLER, D. | AIAA | 1988

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