Книги з теми "Aerodynamics (except hypersonic aerodynamics)"

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

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

Hypersonic flow. New York: Wiley, 1994.

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

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

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

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

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

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

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

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.

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

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

Hypersonic and high-temperature gas dynamics. 2nd ed. Reston, Va: American Institute of Aeronautics and Astronautics, 2006.

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

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.

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

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

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

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

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

NATO Advanced Study Institute on Molecular Physics and Hypersonic Flows (1995 Maretea, Italy). Molecular physics and hypersonic flows: [proceedings of the NATO NATO Advanced Study Institute on Molecular Physics and Hypersonic Flows, Maretea, Italy, May 21-June 3, 1995]. Dordrecht: Kluwer Academic in cooperation with NATO Scientific Affairs Division, 1996.

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

Sehgal, A. K. Investigation of nose bluntness and angle of attack effects on slender bodies in viscous hypertension flows. Norfolk, Va: Dept. of Mechanical Engineering & Mechanics, College of Engineering & Technology, Old Dominion University, 1991.

Shepard, Charles E. Upgrading of NASA-Ames high-energy hypersonic facilities: A study. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1988.

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.

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.

Compendium of NASA Langley reports on hypersonic aerodynamics. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.

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.

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.

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.

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

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.

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.

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.

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

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.

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.

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

S, Murthy T. K. Computational Methods in Hypersonic Aerodynamics. Murthy T K S, 2010.

International Conference on Hypersonic Aerodynamics. The Royal Aeronautical Society, 1989.

Hypersonic and High Temperature Gas Dynamics. AIAA (American Institute of Aeronautics & Ast, 2000.

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.

Turbulence modeling for hypersonic flight. San Jose, CA: MCAT Institute, 1993.

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