Bücher zum Thema „Supersonic / hypersonic“
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Center, Langley Research, Hrsg. Wave-interactions in supersonic and hypersonic flows. Norfolk, Va: Old Dominion University Research Foundation, 1990.
Den vollen Inhalt der Quelle findenLakin, William D. Wave-interactions in supersonic and hypersonic flows. Norfolk, Va: Old Dominion University Research Foundation, 1990.
Den vollen Inhalt der Quelle findenAnderson, Griffin Y. An outlook on hypersonic flight. New York: AIAA, 1987.
Den vollen Inhalt der Quelle findenNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Hypersonic combined cycle propulsion. Neuilly sur Seine, France: AGARD, 1990.
Den vollen Inhalt der Quelle findenNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Hypersonic combined cycle propulsion. Neuilly sur Seine, France: AGARD, 1990.
Den vollen Inhalt der Quelle findenMiles, Richard B. Filtered Rayleigh scattering measurements in supersonic/hypersonic facilities. Washington: AIAA, 1992.
Den vollen Inhalt der Quelle findenCenter, Langley Research, und United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., Hrsg. 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.
Den vollen Inhalt der Quelle findenD, Carboni Jeanne, Supersonic investigation of two dimensional .... und United States. National Aeronautics and Space Administration., Hrsg. Supersonic investigation of two-dimensional hypersonic exhaust nozzles. [Washington, DC: National Aeronautics and Space Administration, 1992.
Den vollen Inhalt der Quelle findenD, Carboni Jeanne, Supersonic investigation of two dimensional... und United States. National Aeronautics and Space Administration., Hrsg. Supersonic investigation of two-dimensional hypersonic exhaust nozzles. [Washington, DC: National Aeronautics and Space Administration, 1992.
Den vollen Inhalt der Quelle findenL, Pittman Jimmy, und United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., Hrsg. 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.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Division., Hrsg. 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.
Den vollen Inhalt der Quelle findenGreene, Francis A. An upwind-biased space marching algorithm for supersonic viscous flow. Hampton, Va: Langley Research Center, 1991.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Division., Hrsg. 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.
Den vollen Inhalt der Quelle findenAnalytical Services & Materials, Inc. und United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., Hrsg. 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.
Den vollen Inhalt der Quelle findenE, Turkel, Abolhassani Jamshid S, Langley Research Center und Institute for Computer Applications in Science and Engineering., Hrsg. 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.
Den vollen Inhalt der Quelle findenRubins, Philip M. A review of supersonic combustion research at AEDC with hypersonic applications. Washington, D. C: American Institute of Aeronautics and Astronautics, 1993.
Den vollen Inhalt der Quelle findenMontagne, 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.
Den vollen Inhalt der Quelle findenAdvisory Group for Aerospace Research and Development. Fluid DynamicsPanel., Advisory Group for Aerospace Research and Development. Consultant and Exchange Programme. und Von Karman Institute for Fluid Dynamics., Hrsg. Special course on three-dimensional supersonic/hypersonic flows including separation. Neuilly sur Seine: Agard, 1990.
Den vollen Inhalt der Quelle findenNorth 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.
Den vollen Inhalt der Quelle findenNorth 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.
Den vollen Inhalt der Quelle findenW, Kniskern Marc, Monta William J und United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., Hrsg. 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.
Den vollen Inhalt der Quelle findenW, Kniskern Marc, Monta William J und United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., Hrsg. 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.
Den vollen Inhalt der Quelle findenHuebner, Lawrence D. Assessment of a flow-through balance for hypersonic wind tunnel models with scramjet exhaust flow simulation. Hampton, Va: Langley Research Center, 1993.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration., Hrsg. Numerical simulation of supersonic and hypersonic inlet flow fields: Final report. Raleigh, N.C: Mars Mission Research Center, North Carolina State University, 1995.
Den vollen Inhalt der Quelle findenE, Melis Matthew, und United States. National Aeronautics and Space Administration., Hrsg. Hypersonic engine leading edge experiments in a high heat flux, supersonic flow environment. [Washington, DC]: National Aeronautics and Space Administration, 1994.
Den vollen Inhalt der Quelle findenCarty, Atherton A. Development and validation of a supersonic helium-air coannular jet facility. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration., Hrsg. An extended supersonic combustion model for the dynamic analysis of hypersonic vehicles. [Washington, DC]: National Aeronautics and Space Administration, 1993.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration., Hrsg. An extended supersonic combustion model for the dynamic analysis of hypersonic vehicles. [Washington, DC]: National Aeronautics and Space Administration, 1993.
Den vollen Inhalt der Quelle findenJ, Wilson Gregory, und United States. National Aeronautics and Space Administration., Hrsg. Computations of axisymmetric flows in hypersonic shock tubes. Washington, DC: American Institute of Aeronautics and Astronautics, 1995.
Den vollen Inhalt der Quelle findenDash, Sanford M. Computational models for the analysis/design of hypersonic scramjet nozzles - Part 1: Combustor and nozzle models. New York: AIAA, 1986.
Den vollen Inhalt der Quelle findenJ, Chattot J., Lawrence S. L und United States. National Aeronautics and Space Administration., Hrsg. 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.
Den vollen Inhalt der Quelle findenNorth 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.
Den vollen Inhalt der Quelle findenNorth 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.
Den vollen Inhalt der Quelle findenAdvisory Group for Aerospace Research and Development. Fluid Dynamics Panel. und Von Karman Institute for FluidDynamics., Hrsg. Special course on shock-wave/boundary-layer interactions in supersonic and hypersonic flows. Neuilly sur Seine: Agard, 1993.
Den vollen Inhalt der Quelle findenA, Mackley Ernest, und Langley Research Center, Hrsg. NASA's hypersonic research engine project: A review. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.
Den vollen Inhalt der Quelle findenCenter, Ames Research, Hrsg. Air-breathing aerospace plane development essential: Hypersonic propulsion flight tests. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1994.
Den vollen Inhalt der Quelle findenMehta, Unmeel B. Air-breathing aerospace plane development essential: Hypersonic propulsion flight tests. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1994.
Den vollen Inhalt der Quelle findenLiu, 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.
Den vollen Inhalt der Quelle findenBaysal, 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.
Den vollen Inhalt der Quelle findenBaysal, Oktay. Viscous computations of cold air/air flow around scramjet nozzle afterbody. Hampton, Va: Langley Research Center, 1991.
Den vollen Inhalt der Quelle findenH, Anderson Bernhard, Shaw Robert J. 1946- und United States. National Aeronautics and Space Administration., Hrsg. Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D code. [Washington, DC]: National Aeronautics and Space Administration, 1994.
Den vollen Inhalt der Quelle findenK, Mikhaĭlov G., und Parton V. Z, Hrsg. Super- and hypersonic aerodynamics and heat transfer. Boca Raton, Fla: CRC Press, 1993.
Den vollen Inhalt der Quelle findenR, Porro A., und United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., Hrsg. 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.
Den vollen Inhalt der Quelle findenL, Semenov Vyacheslav, Hicks John W und Hugh L. Dryden Flight Research Center., Hrsg. 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.
Den vollen Inhalt der Quelle findenL, Semenov Vyacheslav, Hicks John W, Hugh L. Dryden Flight Research Center. und United States. National Aeronautics and Space Administration., Hrsg. 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.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration., Hrsg. Research in robust control for hypersonic vehicles: Progress report #1. Atlanta, Ga: School of Aerospace Engineering, Georgia Institute of Technology, 1992.
Den vollen Inhalt der Quelle findenWitt, Michael A. Investigation in the feasibility of using solid fuel ramjets for high supersonic/low hypersonic tactical missiles. Monterey, Calif: Naval Postgraduate School, 1989.
Den vollen Inhalt der Quelle findenEdwards, 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.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration., Hrsg. Shock-tunnel combustor testing for hypersonic vehicles. San Jose, Calif: MCAT Institute, 1994.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration., Hrsg. Shock-tunnel combustor testing for hypersonic vehicles. San Jose, Calif: MCAT Institute, 1994.
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