Livros sobre o tema "Supersonic / hypersonic"
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Center, Langley Research, ed. Wave-interactions in supersonic and hypersonic flows. Norfolk, Va: Old Dominion University Research Foundation, 1990.
Encontre o texto completo da fonteLakin, William D. Wave-interactions in supersonic and hypersonic flows. Norfolk, Va: Old Dominion University Research Foundation, 1990.
Encontre o texto completo da fonteAnderson, Griffin Y. An outlook on hypersonic flight. New York: AIAA, 1987.
Encontre o texto completo da fonteNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Hypersonic combined cycle propulsion. Neuilly sur Seine, France: AGARD, 1990.
Encontre o texto completo da fonteNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Hypersonic combined cycle propulsion. Neuilly sur Seine, France: AGARD, 1990.
Encontre o texto completo da fonteMiles, Richard B. Filtered Rayleigh scattering measurements in supersonic/hypersonic facilities. Washington: AIAA, 1992.
Encontre o texto completo da fonteCenter, Langley Research, e United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. 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.
Encontre o texto completo da fonteD, Carboni Jeanne, Supersonic investigation of two dimensional .... e United States. National Aeronautics and Space Administration., eds. Supersonic investigation of two-dimensional hypersonic exhaust nozzles. [Washington, DC: National Aeronautics and Space Administration, 1992.
Encontre o texto completo da fonteD, Carboni Jeanne, Supersonic investigation of two dimensional... e United States. National Aeronautics and Space Administration., eds. Supersonic investigation of two-dimensional hypersonic exhaust nozzles. [Washington, DC: National Aeronautics and Space Administration, 1992.
Encontre o texto completo da fonteL, Pittman Jimmy, e United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. 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.
Encontre o texto completo da fonteUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. 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.
Encontre o texto completo da fonteGreene, Francis A. An upwind-biased space marching algorithm for supersonic viscous flow. Hampton, Va: Langley Research Center, 1991.
Encontre o texto completo da fonteUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. 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.
Encontre o texto completo da fonteAnalytical Services & Materials, Inc. e United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. 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.
Encontre o texto completo da fonteE, Turkel, Abolhassani Jamshid S, Langley Research Center e Institute for Computer Applications in Science and Engineering., eds. 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.
Encontre o texto completo da fonteRubins, Philip M. A review of supersonic combustion research at AEDC with hypersonic applications. Washington, D. C: American Institute of Aeronautics and Astronautics, 1993.
Encontre o texto completo da fonteMontagne, 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.
Encontre o texto completo da fonteAdvisory Group for Aerospace Research and Development. Fluid DynamicsPanel., Advisory Group for Aerospace Research and Development. Consultant and Exchange Programme. e Von Karman Institute for Fluid Dynamics., eds. Special course on three-dimensional supersonic/hypersonic flows including separation. Neuilly sur Seine: Agard, 1990.
Encontre o texto completo da fonteNorth 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.
Encontre o texto completo da fonteNorth 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.
Encontre o texto completo da fonteW, Kniskern Marc, Monta William J e United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. 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.
Encontre o texto completo da fonteW, Kniskern Marc, Monta William J e United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. 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.
Encontre o texto completo da fonteHuebner, Lawrence D. Assessment of a flow-through balance for hypersonic wind tunnel models with scramjet exhaust flow simulation. Hampton, Va: Langley Research Center, 1993.
Encontre o texto completo da fonteUnited States. National Aeronautics and Space Administration., ed. Numerical simulation of supersonic and hypersonic inlet flow fields: Final report. Raleigh, N.C: Mars Mission Research Center, North Carolina State University, 1995.
Encontre o texto completo da fonteE, Melis Matthew, e United States. National Aeronautics and Space Administration., eds. Hypersonic engine leading edge experiments in a high heat flux, supersonic flow environment. [Washington, DC]: National Aeronautics and Space Administration, 1994.
Encontre o texto completo da fonteCarty, Atherton A. Development and validation of a supersonic helium-air coannular jet facility. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.
Encontre o texto completo da fonteUnited 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.
Encontre o texto completo da fonteUnited 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.
Encontre o texto completo da fonteJ, Wilson Gregory, e United States. National Aeronautics and Space Administration., eds. Computations of axisymmetric flows in hypersonic shock tubes. Washington, DC: American Institute of Aeronautics and Astronautics, 1995.
Encontre o texto completo da fonteDash, Sanford M. Computational models for the analysis/design of hypersonic scramjet nozzles - Part 1: Combustor and nozzle models. New York: AIAA, 1986.
Encontre o texto completo da fonteJ, Chattot J., Lawrence S. L e United States. National Aeronautics and Space Administration., eds. 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.
Encontre o texto completo da fonteNorth 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.
Encontre o texto completo da fonteNorth 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.
Encontre o texto completo da fonteAdvisory Group for Aerospace Research and Development. Fluid Dynamics Panel. e Von Karman Institute for FluidDynamics., eds. Special course on shock-wave/boundary-layer interactions in supersonic and hypersonic flows. Neuilly sur Seine: Agard, 1993.
Encontre o texto completo da fonteA, Mackley Ernest, e Langley Research Center, eds. NASA's hypersonic research engine project: A review. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.
Encontre o texto completo da fonteCenter, Ames Research, ed. Air-breathing aerospace plane development essential: Hypersonic propulsion flight tests. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1994.
Encontre o texto completo da fonteMehta, Unmeel B. Air-breathing aerospace plane development essential: Hypersonic propulsion flight tests. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1994.
Encontre o texto completo da fonteLiu, 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.
Encontre o texto completo da fonteBaysal, 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.
Encontre o texto completo da fonteBaysal, Oktay. Viscous computations of cold air/air flow around scramjet nozzle afterbody. Hampton, Va: Langley Research Center, 1991.
Encontre o texto completo da fonteH, Anderson Bernhard, Shaw Robert J. 1946- e United States. National Aeronautics and Space Administration., eds. Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D code. [Washington, DC]: National Aeronautics and Space Administration, 1994.
Encontre o texto completo da fonteK, Mikhaĭlov G., e Parton V. Z, eds. Super- and hypersonic aerodynamics and heat transfer. Boca Raton, Fla: CRC Press, 1993.
Encontre o texto completo da fonteR, Porro A., e United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. 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.
Encontre o texto completo da fonteL, Semenov Vyacheslav, Hicks John W e Hugh L. Dryden Flight Research Center., eds. 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.
Encontre o texto completo da fonteL, Semenov Vyacheslav, Hicks John W, Hugh L. Dryden Flight Research Center. e United States. National Aeronautics and Space Administration., eds. 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.
Encontre o texto completo da fonteUnited 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.
Encontre o texto completo da fonteWitt, Michael A. Investigation in the feasibility of using solid fuel ramjets for high supersonic/low hypersonic tactical missiles. Monterey, Calif: Naval Postgraduate School, 1989.
Encontre o texto completo da fonteEdwards, 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.
Encontre o texto completo da fonteUnited States. National Aeronautics and Space Administration., ed. Shock-tunnel combustor testing for hypersonic vehicles. San Jose, Calif: MCAT Institute, 1994.
Encontre o texto completo da fonteUnited States. National Aeronautics and Space Administration., ed. Shock-tunnel combustor testing for hypersonic vehicles. San Jose, Calif: MCAT Institute, 1994.
Encontre o texto completo da fonte