Books on the topic 'Supersonic air inlet'
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Trefny, Charles J. Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets. Cleveland, Ohio: Lewis Research Center, 1986.
Find full textPowell, A. G. Low-speed aerodynamic test of an axisymmetric supersonic inlet with variable cowl slot. [Washington, DC]: National Aeronautics and Space Administration, 1985.
Find full textPowell, A. G. Low-speed aerodynamic test of an axisymmetric supersonic inlet with variable cowl slot. [Washington, DC]: National Aeronautics and Space Administration, 1985.
Find full textPowell, A. G. Low-speed aerodynamic test of an axisymmetric supersonic inlet with variable cowl slot. [Washington, DC]: National Aeronautics and Space Administration, 1985.
Find full textInlets for supersonic missiles. Washington, D.C: American Institute of Aeronautics and Astronautics, 1990.
Find full textHolland, Scott D. Mach 10 experimental database of a three-dimensional scramjet inlet flow field. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.
Find full textFisher, S. A. Internal performance of a variable ramp mixed compression intake at Mach 3.05. Melbourne, Vic: Aeronautical Research Laboratories, 1985.
Find full textW, Wasserbauer Joseph, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.
Find full textW, Wasserbauer Joseph, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.
Find full textUnited States. National Aeronautics and Space Administration., ed. Minimum weight design of a generic axisymmetric inlet. [Washington, DC]: National Aeronautics and Space Administration, 1996.
Find full textJ, Trefny C., and NASA Glenn Research Center, eds. Supersonic wind tunnel tests of a half-axisymmetric 12⁰-spike inlet to a rocket-based combined-cycle propulsion system. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.
Find full textCenter, Langley Research, ed. Mach 10 experimental database of a three-dimensional scramjet inlet flow field. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.
Find full textUnited States. National Aeronautics and Space Administration., ed. Shock-tunnel combustor testing for hypersonic vehicles. San Jose, Calif: MCAT Institute, 1994.
Find full textShock-tunnel combustor testing for hypersonic vehicles. San Jose, Calif: MCAT Institute, 1994.
Find full textUnited States. National Aeronautics and Space Administration., ed. Shock-tunnel combustor testing for hypersonic vehicles. San Jose, Calif: MCAT Institute, 1994.
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