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person:("Miller, D.")

    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

    Research on vtol aircraft handling qualities criteria

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

    Cyclotron resonance propulsion system semiannual report no. 1

    Bethke, G. W. / Miller, D. B. | NTRS | 1965

    Mariner Mars 1964 temperature control subsystem

    Dumas, L. N. / Lewis, D. W. / Miller, D. C. | NTRS | 1967

    Development of liquid oxygen/liquid hydrogen thrust chamber for the M-1 engine

    Barsotti, R. J. / Datsko, S. C. / Kovach, R. J. et al. | NTRS | 1968

    On critical pilot tasks

    Markowitz, J. / Miller, D. C. | NTRS | 1969

    Study of physiological tolerance to centrifugation Final report

    Benedict, J. V. / Miller, D. M. / Nickel, J. A. et al. | NTRS | 1971

    Improved measurement of depth perception

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

    Wreckers and recovery vehicles

    Olyslager Organisation | TIBKAT | 1972
    Contributors: Miller, D. N.

    Refrigeration problems of a VCM-carrying tanker

    Miller, D. | Tema Archive | 1974

    Rubber-tired rapid transit, 1st part: system concepts

    Sulkin, M. / Miller, D. | Tema Archive | 1976

    Rubber-tired rapid transit, part 2: Technical characters

    Sulkin, M. / Miller, D. | Tema Archive | 1976

    Low-frequency vibration isolation

    Miller, D. C. / Otth, D. H. | NTRS | 1978

    Design study results of a supersonic cruise fighter wing

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

      Design study results of a supersonic cruise fighter wing

      Miller, D. S. / Schemensky, R. T. | NTRS | 1979

    The Voyager magnetometer boom

    Miller, D. C. | NTRS | 1979

    Performance verification of an air solar collector

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

    An experimental evaluation of head-up display formats

    Naish, J. M. / Miller, D. L. | NTRS | 1980

    Application Explorer Mission 2 (AEM 2), Stratospheric Aerosol and Gas Experiment (SAGE)

    Mccormick, M. P. / Craig, R. A. / Cunnold, D. M. et al. | NTRS | 1980

    Small self-contained payload overview

    Miller, D. S. | NTRS | 1981

    User needs and the future of operational meteorological satellites

    MILLER, D. / SILVERMAN, J. | AIAA | 1982

      User needs and the future of operational meteorological satellites

      Miller, D. B. / Silverman, J. R. | NTRS | 1982

    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 supersonic maneuver wing designed for nonlinear attached flow

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

      A supersonic maneuver wing designed for nonlinear attached flow

      Mason, W. H. / Siclari, M. J. / Miller, D. S. et al. | NTRS | 1983

    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. | NTRS | 1983

    The stability of an elliptic jet

    MILLER, D. | AIAA | 1984

    Improved Heat-Engine Solar-Energy System

    Miller, D. C. | NTRS | 1984