Książki na temat „Experimental Hypersonic flow”

R, Keener Earl, Hui Frank C. L i Ames Research Center, red. 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 i United States. National Aeronautics and Space Administration., red. 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, red. 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., red. 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., red. 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.