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    An investigation of hypersonic shock tunnel testing at an equilibrium interface condition of 4100 K - Theory and experiment

    MINUCCI, M. / NAGAMATSU, H. | AIAA | 1991

    Experimental investigation of a 2-D scramjet inlet at Mach numbers of 8 to 18 and stagnation temperatures of 4,100K

    MINUCCI, M. / NAGAMATSU, H. | AIAA | 1991

    Laser gain profiles during the nonequilibrium expansion of CO2-N2-Hesystem through a long double-wedge type hypersonic nozzle

    MINUCCI, M. / HINCKEL, J. | AIAA | 1990

    Experimental study of a two-dimensional scramjet at Mach numbers of 8 to 25

    NAGAMATSU, H. / MINUCCI, M. | AIAA | 1990

    Hypersonic shock-tunnel testing at an equilibrium interface condition of 4100 K

    MINUCCI, M. A. S. / NAGAMATSU, H. T. | AIAA | 1993

    Investigation of a two-dimensional scramjet inlet, freestream M = 8-18 and T0 = 4100 K

    MINUCCI, M. A. S. / NAGAMATSU, H. T. | AIAA | 1993

    Combustion shock tunnel and interface compression to produce stagnation temperatures of 20,000 K and Mach numbers of 35

    MINUCCI, M. / NAGAMATSU, H. / MYRABO, L.N. | AIAA | 1992

    Experimental study of a two-dimensional scramjet inset, M(freestream) = 10.1-25.1

    MINUCCI, M. A. S. / NAGAMATSU, H. T. | AIAA | 1992

    Experimental investigation of a 3-D scramjet inlet for laser propulsion at Mach numbers of 10 to 25 and stagnation temperatures of 800 to4100 K

    MYRABO, L. / NAGAMATSU, H. / MINUCCI, M. | AIAA | 1991

    Investigation of a 2-D Scramjet inlet, freestream M = 8.25 and T sub0 = 800-4,100 K

    MINUCCI, M. / NAGAMATSU, H. / KIM, S. | AIAA | 1991

    Experimental pressure investigation of a 'Directed-Energy Air Spike' inlet at Mach 10

    Toro, Paulo / Myrabo, Leik / Nagamatsu, Henry et al. | AIAA | 1999

    Experimental investigation of a 3-D scramjet inlet for laser propulsion at Mach numbers of 8 to 18 and a stagnation temperature of 4100 K

    MYRABO, L. / NAGAMATSU, H. / MINUCCI, M. | AIAA | 1991

    Laser gain measurements in a long noncontoured hypersonic nozzle

    MINUCCI, M. A. S. / HINCKEL, J. N. | AIAA | 1991

    Experimental investigation of an electric arc simulated 'air spike' in hypersonic flow

    Minucci, M. / Bracken, R. / Myrabo, L. et al. | AIAA | 2000

      Experimental Investigation of an Electric Arc Simulated "Air Spike" in Hypersonic Flow

      Minucci, M. A. S. / Bracken, R. M. / Myrabo, L. N. et al. | British Library Conference Proceedings | 2000

    MHD slipstream accelerator investigation in the RPI hypersonic shock tunnel

    Kerl, J. / Myrabo, L. / Nagamatsu, H. et al. | AIAA | 1999

    Computational and experimental investigation of a 2-D scramjet inlet at Mach numbers from 10 to 25

    Messitt, D. / Nagamatsu, H. / Myrabo, L. et al. | AIAA | 1993

      Computational and Experimental Investigation of A 2-D Scramjet Inlet at Mach Numbers From 10 to 25

      Messitt, D. / Nagamatsu, H. / Myrabo, L. et al. | British Library Conference Proceedings | 1993

    Experimental investigation of a 2-D MHD slipstream accelerator and generator

    Meloney, E. / Minucci, M. / Myrabo, L. et al. | AIAA | 2000

    Experimental investigation of a 2-D MHD slipstream generator and accelerator with freestream Mach = 7.6 and T(0) = 4100 K

    Minucci, M. / Meloney, E. / Nagamatsu, H. et al. | AIAA | 2000

    Combustion shock tunnel and interface compression to increase reservoir pressure and enthalpy

    Minucci, M. A. S. / Nagamatsu, H. T. / Myrabo, L. N. | AIAA | 1994

    Adaptive unstructured grid computation for planar flow in a ram accelerator

    Morales, M. / Migueis, C. / Bastos-Netto, D. et al. | AIAA | 1998

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