Books on the topic 'Hypersonic Vehicles'

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

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Flight testing of airbreathing hypersonic vehicles. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

Gerard, Laruelle, Wagner Alain, and United States. National Aeronautics and Space Administration., eds. Systems challenges for hypersonic vehicles: [AGARD] paper C37. [Washington, D.C: National Aeronautics and Space Administration, 1997.

United States. National Aeronautics and Space Administration., ed. Robust intelligent flight control for hypersonic vehicles. Cambridge, Mass: Draper Laboratory, 1992.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Special course on aerothermodynamics of hypersonic vehicles. Neuilly sur Seine, France: AGARD, 1989.

United States. National Aeronautics and Space Administration., ed. Robust intelligent flight control for hypersonic vehicles. Cambridge, Mass: Draper Laboratory, 1992.

United States. National Aeronautics and Space Administration., ed. Shock-tunnel combustor testing for hypersonic vehicles. San Jose, Calif: MCAT Institute, 1994.

United States. National Aeronautics and Space Administration., ed. Shock-tunnel combustor testing for hypersonic vehicles. San Jose, Calif: MCAT Institute, 1994.

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

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

V, Doggett Robert, Ricketts Rodney H, and Langley Research Center, eds. Structural dynamic and aeroelastic considerations for hypersonic vehicles. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

Hirschel, Ernst Heinrich, and Claus Weiland. Selected Aerothermodynamic Design Problems of Hypersonic Flight Vehicles. Berlin, Heidelberg: Springer Berlin Heidelberg, 2009. http://dx.doi.org/10.1007/978-3-540-89974-7.

Claus, Weiland, and American Institute of Aeronautics and Astronautics, eds. Selected aerothermodynamic design problems of hypersonic flight vehicles. Berlin: Springer, 2009.

Y, Chan Samuel, and Langley Research Center, eds. Advanced aerservoelastic stabilization techniques for hypersonic flight vehicles. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

Y, Chan Samuel, and Langley Research Center, eds. Advanced aeroservoelastic stabilization techniques for hypersonic flight vehicles. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

Townend, L. H. Intakes and boundary layer crossflows for hypersonic vehicles. New York: American Institute of Aeronautics and Astronautics, 1991.

S, Chaussee D., Steger Joseph L, and Ames Research Center, eds. Numerical simulation of the hypersonic flow around lifting vehicles. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1987.

S, Chaussee D., Steger Joseph L, and Ames Research Center, eds. Numerical simulation of the hypersonic flow around lifting vehicles. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1987.

Iñigo, Juan Salas. Development of a non-linear simulation for generic hypersonic vehicles -ASUHS1. [Washington, DC: National Aeronautics and Space Administration, 1993.

igo, Juan Salas In. Development of a non-linear simulation for generic hypersonic vehicles -ASUHS1. [Washington, DC: National Aeronautics and Space Administration, 1993.

Center, Langley Research, ed. Review of convectively cooled structures for hypersonic flight. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.

United States. National Aeronautics and Space Administration., ed. Vehicle integration effects on hypersonic waveriders. [Washington, DC: National Aeronautics and Space Administration, 1994.

Stollery, J. L. Hypersonic flow problems associated with future space shuttle vehicles. Cranfield, UK: College of Aeronautics, Cranfield Institute of Technology, 1985.

L, Boman B., and Langley Research Center, eds. Heat pipes for wing leading edges of hypersonic vehicles. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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.

Bogdonoff, Seymour M. Technical evaluation report on the Fluid Dynamics Panel Symposium on Aerodynamics of Hypersonic Lifting Vehicles. Neuilly sur Seine, France: AGARD, 1988.

G, Hornung H., Whitehead R. E, and North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development., eds. Technical evaluation report on the Fluid Dynamics Panel Symposium on Aerodynamics of Hypersonic Lifting Vehicles. Neuilly sur Seine, France: AGARD, 1988.

Salemann, Victor. Propulsion system integration for Mach 4 to 6 vehicles. [New York]: American Institute of Aeronautics and Astronautics, 1988.

United States. National Aeronautics and Space Administration., ed. Research in robust control for hypersonic vehicles: Progress report #1. Atlanta, Ga: School of Aerospace Engineering, Georgia Institute of Technology, 1992.

D, Stein Matthew, and United States. National Aeronautics and Space Administration., eds. Configuration development study of the OSU I hypersonic research vehicles. [Columbus, Ohio]: Ohio State State University, 1993.

M, Gregory Irene, and Langley Research Center, eds. Trim drag reduction concepts for horizontal takeoff single-stage-to-orbit vehicles. Hampton, VA: National Aeronautics and Space Administration, Langley Research Center, 1991.

J, Baumgarten William, Alexander Stephen W, and United States. National Aeronautics and Space Administration., eds. Mission and sizing analysis for the Beta II two-stage-to-orbit vehicle. Washington, DC: National Aeronautics and Space Administration, 1992.

Messitt, D. G. Comparison between computational and experimental data for a hypersonic laser propelled vehicle. Washington, D. C: American Institute of Aeronautics and Astronautics, 1992.

J, Baumgarten William, Alexander Stephen W, and United States. National Aeronautics and Space Administration., eds. Mission and sizing analysis for the Beta II two-stage-to-orbit vehicle. Washington, DC: National Aeronautics and Space Administration, 1992.

United States. National Aeronautics and Space Administration., ed. A parametric sensitivity study for single-stage-to-orbit hypersonic vehicles using trajectory optimization. College Park, Md: Dept. of Aerospace Engineering, University of Maryland, 1994.

N, Gupta Roop, and Langley Research Center, eds. Viscous-shock-layer analysis of hypersonic flows over long slender vehicles. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

N, Gupta Roop, and Langley Research Center, eds. Viscous-shock-layer analysis of hypersonic flows over long slender vehicles. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

N, Gupta Roop, and Langley Research Center, eds. Viscous-shock-layer analysis of hypersonic flows over long slender vehicles. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

D, Freeman, and United States. National Aeronautics and Space Administration., eds. The NASA Hyper-X Program. Paris, France: International Astronautical Federation, 1997.

IUTAM Symposium on Aerothermochemistry of Spacecraft and Associated Hypersonic Flows (1992 Marseille, France). Aerothermochemistry of spacecraft and associated hypersonic flows: Proceedings of the IUTAM Symposium held in Marseille, France, Le Palais du Pharo, September 1-4, 1992. [France: s.n.], 1994.

Harloff, G. J. HASA, Hypersonic Aerospace Sizing Analysis, for the preliminary design of aerospace vehicles. [Washington, DC]: National Aeronautics and Space Administration, 1989.

Mehta, Unmeel B. Synthesis of contributed simulations for OREX test cases. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1998.

Vermeulen, J. P. Parametric studies of shock wave/boundary layer interactions over 2D compression corners at Mach 6. Rhode Saint Genese, Belgium: von Karman Institute for Fluid Dynamics, 1992.

United States. National Aeronautics and Space Administration., ed. An extended supersonic combustion model for the dynamic analysis of hypersonic vehicles. [Washington, DC]: National Aeronautics and Space Administration, 1993.

United States. National Aeronautics and Space Administration., ed. An extended supersonic combustion model for the dynamic analysis of hypersonic vehicles. [Washington, DC]: National Aeronautics and Space Administration, 1993.

United States. National Aeronautics and Space Administration., ed. Guidance and flight control law development for hypersonic vehicles: Progress report, #3, reporting period, 7-5-92 - 1-31-93. Athens, Ga: School of Aerospace Engineering, Georgia Institute of Technology, 1993.

N, Moss James, Scott Carl D, American Institute of Aeronautics and Astronautics., AIAA Aerospace Sciences Meeting (23rd : 1985 : Reno, Nev.), and AIAA Thermophysics Conference (20th : 1985 : Williamsburg, Va.), eds. Thermophysical aspects of re-entry flows. New York, NY: American Institute of Aeronautics and Astronautics, Inc., 1986.

F, Covell Peter, Forrest Dana K, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

Zheng-Tao, Deng, and United States. National Aeronautics and Space Administration., eds. Exhausted plume flow field prediction near the afterbody of hypersonic flight vehicles in high altitudes. [Washington, D.C: National Aeronautics and Space Administration, 1995.

Baysal, Oktay. Viscous computations of cold air/airflow around scramjet nozzle afterbody. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.