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Academic literature on the topic 'Experimental Hypersonic flow'
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Books on the topic "Experimental Hypersonic flow"
R, Keener Earl, Hui Frank C. L, and Ames Research Center, eds. Experimental results for a hypersonic nozzle/afterbody flow field. National Aeronautics and Space Administration, Ames Research Center, 1995.
Find full textHughson, M. C. Hypersonic prediction comparisons with experimental data for a cone-cylinder at Mach 6.86. Air Force Armament Laboratory, Eglin Air Force Base, 1989.
Find full textW, Paulson John, Weilmuenster K. James, and United States. National Aeronautics and Space Administration., eds. Experimental and computational analysis of shuttle orbiter hypersonic trim anomaly. American Institute of Aeronautics and Astronautics, 1995.
Find full textNagamatsu, Henry T. Computational, theoretical, and experimental investigation of flow over a sharp flat plate, M1 = 10 - 25. American Institute of Aeronautics and Astronautics, 1994.
Find full textCenter, Langley Research, ed. Mach 10 experimental database of a three-dimensional scramjet inlet flow field. National Aeronautics and Space Administration, Langley Research Center, 1995.
Find full textHolland, Scott D. Mach 10 experimental database of a three-dimensional scramjet inlet flow field. National Aeronautics and Space Administration, Langley Research Center, 1995.
Find full textUnited States. National Aeronautics and Space Administration., ed. Experimental aerothermodynamic research of hypersonic aircraft: Technical progress report (substitution) for the period October 1, 1988 - March 31, 1989. National Aeronautics and Space Administration, 1989.
Find full textUnited States. National Aeronautics and Space Administration., ed. Experimental aerothermodynamic research of hypersonic aircraft: Technical progress report (substitution) for the period March 1, 1987 - September 30, 1987. National Aeronautics and Space Administration, 1987.
Find full textAvery, Don E. Experimental aerodynamic heating to simulated space shuttle tiles in laminar and turbulent boundary layers with variable flow angles at a nominal Mach number of 7. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
Find full textWells, William L. Surface flow and heating distributions on a cylinder in near wake of Aeroassist Flight Experiment (AFE) configuration at incidence in Mach 10 air. Langley Research Center, 1990.
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