Books on the topic 'Hypersonic'

Hypersonic flow. New York: Wiley, 1994.

HEPPENHEIMER, T. A. Hypersonic technologies. Arlington, Va: Pasha Publications, 1993.

Hypersonic aerothermodynamics. Washington, DC: American Institute of Aeronautics and Astronautics, 1994.

Park, Chul. Nonequilibrium hypersonic aerothermodynamics. New York: Wiley, 1990.

T, Pratt David, ed. Hypersonic airbreathing propulsion. Washington, D.C: American Institute of Aeronautics and Astronautics, 1994.

Griffith, Wayland C. Hypersonic nozzle design. Raleigh, N. C: North Carolina State University, 1989.

Hani, Alkamhawi, and United States. National Aeronautics and Space Administration., eds. Hypersonic aircraft design. [Columbus, Ohio]: Ohio State University, 1990.

Bruno, Claudio. Airbreathing Hypersonic Propulsion. Singapore: Springer Nature Singapore, 2023. http://dx.doi.org/10.1007/978-981-19-7927-9.

L, Rausch Vincent, and United States. National Aeronautics and Space Administration., eds. Airbreathing hypersonic systems focus at NASA Langley Research Center. Washington, DC: American Institute of Aeronautics and Astronautics, 1998.

N, Pessin David, and Ames Research Center, eds. Aerodynamic analysis of hypersonic waverider aircraft. San Luis Obispo, CA: Cal Poly State University, 1993.

United States. National Aeronautics and Space Administration., ed. Aerodynamic heating rate distributions induced by trailing edge controls on hypersonic aircraft configurations at Mach 8. [Washington, DC?: National Aeronautics and Space Administration, 1985.

McCandless, Ronald S. Hypersonic characteristics of an advanced aerospace plane at Mach 20.3. Washington, D.C: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

Richard, Hallion, Schweikart Larry, and Air Force History and Museums Program (U.S.), eds. The hypersonic revolution: Case studies in the history of hypersonic technology. Bolling AFB, D.C: Air Force History and Museums Program, 1998.

Richard, Hallion, and Air Force History and Museums Program (U.S.), eds. The Hypersonic revolution: Case studies in the history of hypersonic technology. Bolling AFB, DC: Air Force History and Museums Program, 1998.

Sheng, Yi Qian. Hypersonic inlet flow computation. Ottawa: National Library of Canada, 1992.

Morkovin, Mark Vladimir. Transition at hypersonic speeds. Hampton, Va: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1987.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Hypersonic combined cycle propulsion. Neuilly sur Seine, France: AGARD, 1990.

Center, Lewis Research, ed. CFD for hypersonic propulsion. [Cleveland, Ohio: Lewis Research Center, 1991.

K, Lu Frank, and Marren Dan E, eds. Advanced hypersonic test facilities. Reston, Va: American Institute of Aeronautics and Astronautics, 2002.

Jacobi, L. Y. I.A.I. hypersonic wind tunnel. Ben Gurion Airport, Israel: Israel Aircraft Industries Ltd, 1987.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Hypersonic combined cycle propulsion. Neuilly sur Seine, France: AGARD, 1990.

Morkovin, Mark Vladimir. Transition at hypersonic speeds. Hampton, Va: ICASE, 1987.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Hypersonic rarefied wake characterization. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

Simeonides, G. The performance of the VKI Longshot hypersonic wind tunnel. Rhode Saint Genese, Belgium: von Karman Institute for Fluid Dynamics, 1987.

Ahuja, J. K. Investigation of hypersonic shock-induced combustion in a hydrogen-air system. Washington, D. C: American Institute of Aeronautics and Astronautics, 1992.

N, Tiwari S., Singh D. J, and Old Dominion University. Dept. of Mechanical Engineering and Mechanics., eds. Investigation of hypersonic shock-induced combustion in a hydrogen-air system. Norfolk, Va: Old Dominion University Research Foundation, 1992.

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.

Richard, Hallion, Becker John Vernon 1913-, and United States. Air Force. Systems Command. Aeronautical Systems Division. Special Staff Office, eds. The Hypersonic revolution: Eight case studies in the history of hypersonic technology. Wright-Patterson Air Force Base, Ohio: Special Staff Office, Aeronautical Systems Division, 1987.

Richard, Hallion, Becker John Vernon 1913-, and United States. Air Force. Systems Command. Aeronautical Systems Division. Special Staff Office., eds. The Hypersonic revolution: Eight case studies in the history of hypersonic technology. Wright-Patterson Air Force Base, Ohio: Special Staff Office, Aeronautical Systems Division, 1987.

Radespiel, R. Progress with multigrid schemes for hypersonic flow problems. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

Anderson, John David. Hypersonic and high temperature gas dynamics. New York: McGraw-Hill, 1989.

Flandro, G. A. Dynamic interactions between hypersonic vehicle aerodynamics and propulsion system performance: Final report to Aircraft Guidance and Controls Branch, Guidance and Control Division ... [Washington, DC: National Aeronautics and Space Administration, 1992.

United States. National Aeronautics and Space Administration., ed. Advanced computational techniques for hypersonic propulsion. [Washington, DC]: National Aeronautics and Space Administration, 1989.

Heinrich, Ralf. Berechnung stationärer Hyperschallströmungen unter Verwendung eines zonalen Konzeptes. Aachen: Shaker, 1996.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. Aerodynamic pressures and heating rates on surfaces between split elevons at Mach 6.6. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

United States. National Aeronautics and Space Administration., ed. Particle kinetic simulation of high altitude hypervelocity flight: Periodic research report, cooperative agreement NCC2-582 for the period January 1, 1993 - August 31, 1993. [Washington, DC: National Aeronautics and Space Administration, 1993.

Tannehill, John C. Development of a 3-D upwind PNS code for chemically reacting hypersonic flowfields. [Washington, DC: National Aeronautics and Space Administration, 1992.

United States. National Aeronautics and Space Administration., ed. Hypersonic aerodynamic coefficients and convection flow estimation in a Hermes type project. Washington, DC: National Aeronautics and Space Administration, 1987.

Tannehill, John C. Development of a 3-D upwind PNS code for chemically reacting hypersonic flowfields. [Washington, DC: National Aeronautics and Space Administration, 1992.

Philip, Hall, and Langley Research Center, eds. Nonlinear development and secondary instability of Görtler vortices in hypersonic flows. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

United States. National Aeronautics and Space Administration., ed. Power-on performance predictions for a complete generic hypersonic vehicle configuration. San Jose, CA: MCAT Institute, 1991.

K, Schmidt D., and United States. National Aeronautics and Space Administration., eds. Generic hypersonic vehicle performance model: Interim task report for NASA grant NAG-1-1341. [Washington, DC: National Aeronautics and Space Administration, 1993.

L, Rasmussen Maurice, and United States. National Aeronautics and Space Administration., eds. Computational analysis of hypersonic flows past elliptic-cone waveriders. [Norman, Okla.]: University of Oklahoma, School of Aerospace and Mechanical Engineering, 1991.

Center, Langley Research, ed. A study of viscous interaction effects on hypersonic waveriders. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

United States. National Aeronautics and Space Administration., ed. Power-on performance predictions for a complete generic hypersonic vehicle configuration. San Jose, CA: MCAT Institute, 1991.

Center, Ames Research, ed. Maximum lift/drag ratio of flat plates with bluntness and skin friction at hypersonic speeds. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1987.

United States. National Aeronautics and Space Administration., ed. A test fixture for measuring high-temperature hypersonic-engine seal performance. [Washington, DC]: National Aeronautics and Space Administration, 1991.

G, Wadawadigi, and United States. National Aeronautics and Space Administration., eds. Development of a 3-D upwind PNS code for chemically reacting hypersonic flowfields: Final report : NASA grant NAG 2-502, February 1, 1988--January 31, 1992. [Washington, DC: National Aeronautics and Space Administration, 1992.

Center, Langley Research, ed. A study of viscous interaction effects on hypersonic waveriders. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

Real gas flows with high velocities. Boca Raton: Taylor & Francis, 2009.