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AIAA   MILLER, D.   PITTMAN, J.   MASON, W.   Verkehrstechnik, Verkehrswesen   Physik   Elektrotechnik   Auswahl aufheben
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    Directional filters for sensing 1-D structural dynamics

    PINES, D. / MILLER, D. / VON FLOTOW, A. | AIAA | 1992

    Rotating disk oxygen generator

    HARPOLE, G. / ENGLISH, W. / BERG, J. et al. | AIAA | 1992

    Development of spatially convolving sensors for structural control applications

    MILLER, D. / COLLINS, S. | AIAA | 1990

    Flight hardware and tele-operations supporting the Isothermal Dendritic Growth Experiment aboard the Space Shuttle

    WINSA, E. / KRAFT, G. / GLICKSMAN, M. et al. | AIAA | 1989

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

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

    Large-scale turbulence structuring in high Reynolds number flows

    DE JONCKHEERE, R. / CHOU, D. / MILLER, D. et al. | AIAA | 1988

    Combined structural and control optimization for flexible systems using gradient based searches

    MILLER, D. / SHIM, J. | AIAA | 1986

    Application of NCOREL to conical multi-finned and multi-faceted configurations

    SICLARI, M. / MILLER, D. | AIAA | 1986

    An evaluation of leading-edge flap performance on delta and double-delta wings at supersonic speeds

    COVELL, P. / MILLER, D. / WOOD, R. | AIAA | 1986

    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

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

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

    A comparison of experimental and numerical results for delta wings with vortex flaps

    POWELL, K. / MURMAN, E. / WOOD, R. et al. | AIAA | 1986

    Impact of airfoil profile on the supersonic aerodynamics of delta wings

    WOOD, R. / MILLER, D. | AIAA | 1985

    Aerodynamic design considerations for efficient high-lift supersonicwings

    MILLER, D. / WOOD, R. | AIAA | 1985

    Inertial actuator design for maximum passive and active energy dissipation in flexible space structures

    MILLER, D. / CRAWLEY, E. / WARD, B. | AIAA | 1985

    The stability of an elliptic jet

    MILLER, D. | AIAA | 1984

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

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

    Impact of fuselage incidence on the supersonic aerodynamics of two fighter configurations

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

    An investigation of wing leading-edge vortices at supersonic speeds

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

    An overview of two nonlinear supersonic wing design studies

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

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