Książki na temat „Supersonic / hypersonic”

Center, Langley Research, red. Wave-interactions in supersonic and hypersonic flows. Norfolk, Va: Old Dominion University Research Foundation, 1990.

Lakin, William D. Wave-interactions in supersonic and hypersonic flows. Norfolk, Va: Old Dominion University Research Foundation, 1990.

Anderson, Griffin Y. An outlook on hypersonic flight. New York: AIAA, 1987.

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.

Miles, Richard B. Filtered Rayleigh scattering measurements in supersonic/hypersonic facilities. Washington: AIAA, 1992.

Center, Langley Research, i United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., red. Nonparallel instability of supersonic and hypersonic boundary layers. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.

D, Carboni Jeanne, Supersonic investigation of two dimensional .... i United States. National Aeronautics and Space Administration., red. Supersonic investigation of two-dimensional hypersonic exhaust nozzles. [Washington, DC: National Aeronautics and Space Administration, 1992.

D, Carboni Jeanne, Supersonic investigation of two dimensional... i United States. National Aeronautics and Space Administration., red. Supersonic investigation of two-dimensional hypersonic exhaust nozzles. [Washington, DC: National Aeronautics and Space Administration, 1992.

L, Pittman Jimmy, i United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., red. Aerodynamic characteristics of a distinct wing-body configuration at Mach 6: Experiment, theory, and the hypersonic isolation principle. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., red. An upwind-biased space marching algorithm for supersonic viscous flow. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.

Greene, Francis A. An upwind-biased space marching algorithm for supersonic viscous flow. Hampton, Va: Langley Research Center, 1991.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., red. An upwind-biased space marching algorithm for supersonic viscous flow. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.

Analytical Services & Materials, Inc. i United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., red. Secondary instability of high-speed flows and the influence of wall cooling and suction. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

E, Turkel, Abolhassani Jamshid S, Langley Research Center i Institute for Computer Applications in Science and Engineering., red. Extension of multigrid methodology to supersonic/hypersonic 3-D viscous flows. Hampton, Va: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1991.

Rubins, Philip M. A review of supersonic combustion research at AEDC with hypersonic applications. Washington, D. C: American Institute of Aeronautics and Astronautics, 1993.

Montagne, J. L. Recherches fondamentales sur des methodes de calcul pour des ecoulements supersoniques et hypersoniques. Paris: Office national d'etudes et de recherches aerospatiales. Direction de l'aerodynamique, 1985.

Advisory Group for Aerospace Research and Development. Fluid DynamicsPanel., Advisory Group for Aerospace Research and Development. Consultant and Exchange Programme. i Von Karman Institute for Fluid Dynamics., red. Special course on three-dimensional supersonic/hypersonic flows including separation. Neuilly sur Seine: Agard, 1990.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Special course on three-dimensional supersonic/hypersonic flows including separation. Neuilly-sur-Seine: AGARD, 1990.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Special course on three-dimensional supersonic/hypersonic flows including separation. Neuilly sur Seine, France: AGARD, 1990.

W, Kniskern Marc, Monta William J i United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., red. Assessment of a flow-through balance for hypersonic wind tunnel models with scramjet exhaust flow simulation. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

W, Kniskern Marc, Monta William J i United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., red. Assessment of a flow-through balance for hypersonic wind tunnel models with scramjet exhaust flow simulation. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

Huebner, Lawrence D. Assessment of a flow-through balance for hypersonic wind tunnel models with scramjet exhaust flow simulation. Hampton, Va: Langley Research Center, 1993.

United States. National Aeronautics and Space Administration., red. Numerical simulation of supersonic and hypersonic inlet flow fields: Final report. Raleigh, N.C: Mars Mission Research Center, North Carolina State University, 1995.

E, Melis Matthew, i United States. National Aeronautics and Space Administration., red. Hypersonic engine leading edge experiments in a high heat flux, supersonic flow environment. [Washington, DC]: National Aeronautics and Space Administration, 1994.

Carty, Atherton A. Development and validation of a supersonic helium-air coannular jet facility. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

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

J, Wilson Gregory, i United States. National Aeronautics and Space Administration., red. Computations of axisymmetric flows in hypersonic shock tubes. Washington, DC: American Institute of Aeronautics and Astronautics, 1995.

Dash, Sanford M. Computational models for the analysis/design of hypersonic scramjet nozzles - Part 1: Combustor and nozzle models. New York: AIAA, 1986.

J, Chattot J., Lawrence S. L i United States. National Aeronautics and Space Administration., red. Parallelization of a parabolized Navier-Stokes solver with a design optimizer: 34th AIAA Aerospace Sciences Meeting and Exhibit. [Washington, DC: National Aeronautics and Space Administration, 1996.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Special course on shock-wave/boundary-layer interactions in supersonic and hypersonic flows. Neuilly-sur-Seine: AGARD, 1993.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Special course on shock wave boundary layer interactions in supersonic and hypersonic flows. Neuilly-sur-Seine, France: AGARD, 1993.

Advisory Group for Aerospace Research and Development. Fluid Dynamics Panel. i Von Karman Institute for FluidDynamics., red. Special course on shock-wave/boundary-layer interactions in supersonic and hypersonic flows. Neuilly sur Seine: Agard, 1993.

A, Mackley Ernest, i Langley Research Center, red. NASA's hypersonic research engine project: A review. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

Center, Ames Research, red. Air-breathing aerospace plane development essential: Hypersonic propulsion flight tests. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1994.

Mehta, Unmeel B. Air-breathing aerospace plane development essential: Hypersonic propulsion flight tests. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1994.

Liu, Shiao-kung. Aerospace-plane flights and stratospheric ozone: Review and preliminary assessment of the National Aerospace Plane (NASP) operations. Santa Monica, CA: Rand Corporation, 1992.

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.

Baysal, Oktay. Viscous computations of cold air/air flow around scramjet nozzle afterbody. Hampton, Va: Langley Research Center, 1991.

H, Anderson Bernhard, Shaw Robert J. 1946- i United States. National Aeronautics and Space Administration., red. Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D code. [Washington, DC]: National Aeronautics and Space Administration, 1994.

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

R, Porro A., i United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., red. Evaluation of a technique to generate artificially thickened boundary layers in supersonic and hypersonic flows. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.

L, Semenov Vyacheslav, Hicks John W i Hugh L. Dryden Flight Research Center., red. Recent flight test results of the joint CIAM-NASA Mach 6.5 Scramjet Flight Program. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1998.

L, Semenov Vyacheslav, Hicks John W, Hugh L. Dryden Flight Research Center. i United States. National Aeronautics and Space Administration., red. Recent flight test results of the joint CIAM-NASA Mach 6.5 Scramjet Flight Program. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1998.

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

Witt, Michael A. Investigation in the feasibility of using solid fuel ramjets for high supersonic/low hypersonic tactical missiles. Monterey, Calif: Naval Postgraduate School, 1989.

Edwards, Thomas A. The effect of exhaust plume/afterbody interaction on installed scramjet performance. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1988.

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

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