Книги з теми "Experimental Hypersonic flow"

R, Keener Earl, Hui Frank C. L, and Ames Research Center, eds. Experimental results for a hypersonic nozzle/afterbody flow field. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1995.

Hughson, M. C. Hypersonic prediction comparisons with experimental data for a cone-cylinder at Mach 6.86. Eglin Air Force Base, Fl: Air Force Armament Laboratory, Eglin Air Force Base, 1989.

W, Paulson John, Weilmuenster K. James, and United States. National Aeronautics and Space Administration., eds. Experimental and computational analysis of shuttle orbiter hypersonic trim anomaly. Washington, DC: American Institute of Aeronautics and Astronautics, 1995.

Nagamatsu, Henry T. Computational, theoretical, and experimental investigation of flow over a sharp flat plate, M1 = 10 - 25. Washington, D. C: American Institute of Aeronautics and Astronautics, 1994.

Center, 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.

Holland, 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.

United 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. [Washington, DC: National Aeronautics and Space Administration, 1989.

United 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. [Washington, DC: National Aeronautics and Space Administration, 1987.

Avery, 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. Washington, D.C: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

Wells, 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. Hampton, Va: Langley Research Center, 1990.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Fluid Dynamics Panel. Symposium. Theoretical and experimental methods in hypersonic flows =: Les méthodes théoriques et expérimentales pour l'etude des ecoulements hypersoniques. Neuilly sur Seine, France: AGARD, 1993.

Development, North Atlantic Treaty Organization Advisory Group for Aerospace Research and. Theoretical and experimental methods in hypersonic flows: Papers presented and discussions held at the Fluid Dynamics Panel Symposium held in Torino, Italy, from 4th-8th May 1992. Neuilly-sur-Seine: AGARD, 1993.

Experimental studies of shock-wave/wall-jet interaction in hypersonic flow. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

Experimental and computational analysis of shuttle orbiter hypersonic trim anomaly. Washington, DC: American Institute of Aeronautics and Astronautics, 1995.

A computational and experimental investigation of a three-dimensional hypersonic scramjet inlet flow field. Raleligh, NC: North Carolina State University, 1991.

Nelson, Wilbur C. High Temperature Aspects of Hypersonic Flow: Proceedings of the AGARD-NATO Specialists' Meeting Sponsored by the Fluid Dynamics Panel of Agard Held at the Technical Centre for Experimental Aerodynamics, Rhode-Saint-Genèse, Belgium, 3-6 April 1962. Elsevier Science & Technology Books, 2014.