Books on the topic 'Hypersonic Aerodynamics'

K, Notestine Kristopher, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Aerodynamic pressure and heating-rate distributions in tile gaps around chine regions with pressure gradients at a Mach number of 6.6. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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

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

S, Murthy T. K., ed. Computational methods in hypersonic aerodynamics. Southampton: Computational Mechanics Publications, 1991.

Utyuzhnikov, Sergey V. Hypersonic aerodynamics and heat transfer. New York: Begell, 2014.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Aerodynamics of Hypersonic Lifting Vehicles. S.l: s.n, 1987.

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

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.

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.

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.

Anderson, John David. Hypersonic and high-temperature gas dynamics. 2nd ed. Reston, VA: AIAA, 2007.

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

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.

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

Cruz, Christopher I. Improved tangent-cone method for the Aerodynamic Preliminary Analysis System (APAS) version of the Hypersonic Arbitrary-Body Program. Hampton, Va: Langley Research Center, 1990.

J, Sova Gregory, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Improved tangent-cone method for the Aerodynamic Preliminary Analysis System (APAS) version of the hypersonic arbitrary-body program. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

United States. National Aeronautics and Space Administration., ed. Turbulence modeling for hypersonic flight. San Jose, CA: MCAT Institute, 1992.

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.

K, Mikhaĭlov G., and Parton V. Z, eds. Super- and hypersonic aerodynamics and heat transfer. Boca Raton, Fla: CRC Press, 1993.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Pitot survey of exhaust flow field of a 2-D scramjet nozzle at Mach 6 with air or freon and argon used for exhaust simulation. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

1945-, Harloff G. J., and Lewis Research Center, eds. Hypersonic turbulent wall boundary layer computations. Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1988.

United States. National Aeronautics and Space Administration., ed. Evaluation of an innovative high temperature ceramic wafer seal for hypersonic engine applications. [Washington, DC]: National Aeronautics and Space Administration, 1992.

United States. National Aeronautics and Space Administration., ed. Computation of H2/air reacting flowfields in drag-reduction external combustion. [Washington, DC: National Aeronautics and Space Administration, 1992.

Liu, S. K. Numerical simulation of hypersonic aerodynamics and the computational needs for the design of an aerospace plane. Santa Monica, Calif: Rand, 1992.

Simon, Donald L. A high-frequency servosystem for fuel control in hypersonic engines. [Washington, DC]: National Aeronautics and Space Administration, 1991.

N, Gupta Roop, Shinn Judy L, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Conservation equations and physical models for hypersonic air flows in thermal and chemical equilibrium. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

H, Klopfer Goetz, Montagne J. -L, and Ames Research Center, eds. High-resolution shock-capturing schemes for inviscid and viscous hypersonic flows. Moffet Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1988.

Center, Langley Research, ed. A High angle of attack inviscid shuttle orbiter computation. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

Center, Langley Research, ed. Studies of aerothermal loads generated in regions of shock/shock interaction in hypersonic flow. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.