Bücher zum Thema „Wave turbulence interaction“
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Milewski, Paul A., Leslie M. Smith, Fabian Waleffe und Esteban G. Tabak, Hrsg. Advances in Wave Interaction and Turbulence. Providence, Rhode Island: American Mathematical Society, 2001. http://dx.doi.org/10.1090/conm/283.
Der volle Inhalt der QuelleLee, Sangsan. Interaction of isotropic turbulence with a shock wave. Stanford, Calif: Thermo sciences Division, Dept. of Mechanical Engineering, Stanford University, 1992.
Den vollen Inhalt der Quelle findenRibner, Herbert S. Spectrum of noise from shock-turbulence interaction. [S.l.]: [s.n.], 1986.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration., Hrsg. A simple theory of capillary-gravity wave turbulence. [Washington, DC: National Aeronautics and Space Administration, 1995.
Den vollen Inhalt der Quelle findenRubinstein, Robert. The dissipation range in rotating turbulence. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1999.
Den vollen Inhalt der Quelle findenKim, S. W. Numerical computation of shock wave-turbulent boundary layer interaction in transonic flow over an axisymmetric curved hill. Cleveland, Ohio: Lewis Research Center, 1989.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration. und Lewis Research Center. Institute for Computational Mechanics in Propulsion., Hrsg. Numerical investigation of separated transonic turbulent flows with a multiple-time-scale turbulence model. [Washington, D.C: National Aeronautics and Space Administration, 1990.
Den vollen Inhalt der Quelle finden1931-, Toba Y., Mitsuyasu Hisashi 1929-, IOC/SCOR Committee on Climatic Changes and the Ocean., WMO/ICSU Joint Scientific Committee. und Symposium on Wave Breaking, Turbulent Mixing and Radio Probing of the Ocean Surface (1984 : Tohoku University), Hrsg. The Ocean surface: Wave breaking, turbulent mixing, and radio probing. Dordrecht [Netherlands]: Reidel, 1985.
Den vollen Inhalt der Quelle findenAMS-IMS-SIAM Joint Summer Research Conference on Dispersive Wave Turbulence (2000 Mount Holyoke College). Advances in wave interaction and turbulence: Proceedings of an AMS-IMS-SIAM Joint Summer Research Conference on Dispersive Wave Turbulence, Mount Holyoke College, South Hadley, MA, June 11-15, 2000. Herausgegeben von Milewski Paul A. 1966-. Providence, R.I: American Mathematical Society, 2001.
Den vollen Inhalt der Quelle findenCenter, Langley Research, Hrsg. Laminar and turbulent flow computations of type IV shock-shock interference aerothermal loads using unstructured grids. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.
Den vollen Inhalt der Quelle findenCenter, Langley Research, Hrsg. Laminar and turbulent flow computations of type IV shock-shock interference aerothermal loads using unstructured grids. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.
Den vollen Inhalt der Quelle findenK, Wideman J., und United States. National Aeronautics and Space Administration., Hrsg. Skin-friction measurements in a 3-D, supersonic shock-wave/boundary-layer interaction: 32nd Aerospace Sciences Meeting & Exhibit, January 10-13, 1994/Reno, NV. Washington, D.C: American Institute of Aeronautics and Astronautics, 1994.
Den vollen Inhalt der Quelle findenK, Wideman J., und United States. National Aeronautics and Space Administration., Hrsg. Skin-friction measurements in a 3-D, supersonic shock-wave/boundary-layer interaction: 32nd Aerospace Sciences Meeting & Exhibit, January 10-13, 1994/Reno, NV. Washington, D.C: American Institute of Aeronautics and Astronautics, 1994.
Den vollen Inhalt der Quelle findenK, Wideman J., und United States. National Aeronautics and Space Administration., Hrsg. Skin-friction measurements in a 3-D, supersonic shock-wave/boundary-layer interaction: 32nd Aerospace Sciences Meeting & Exhibit, January 10-13, 1994/Reno, NV. Washington, D.C: American Institute of Aeronautics and Astronautics, 1994.
Den vollen Inhalt der Quelle findenSpring College on Plasma Physics (1993 Trieste, Italy). Wave-particle interaction and energization in plasmas: Proceedings of the 4th week of the Spring College on Plasma Physics : Trieste, Italy, June 7-11, 1993. Herausgegeben von Shukla P. K. Stockholm: Royal Swedish Academy of Sciences, 1994.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration., Hrsg. Turbulence modeling in shock wave/turbulent boundary layer interactions: Final report. [Washington, DC: National Aeronautics and Space Administration, 1992.
Den vollen Inhalt der Quelle findenCenter, Ames Research, Hrsg. Turbulence modeling for sharp-fin-induced shock wave/turbulent boundary-layer interactions. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1990.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration., Hrsg. Computational modeling and validation for hypersonic inlets. [Washington, D.C: National Aeronautics and Space Administration, 1990.
Den vollen Inhalt der Quelle findenDélery, J., Hrsg. Turbulent Shear-Layer/Shock-Wave Interactions. Berlin, Heidelberg: Springer Berlin Heidelberg, 1986. http://dx.doi.org/10.1007/978-3-642-82770-9.
Der volle Inhalt der QuelleIUTAM Symposium (1985 Palaiseau, France). Turbulent shear-layer/shock-wave interactions. Herausgegeben von Délery J. 1939-, International Union of Theoretical and Applied Mechanics. und France. Office national d'études et de recherches aérospatiales. Berlin: Springer-Verlag, 1986.
Den vollen Inhalt der Quelle findenMankbadi, Reda R. Multiwave interactions in turbulent jets. Cleveland, Ohio: Institute for Computational Mechanics in Propulsion, 1989.
Den vollen Inhalt der Quelle findenKussoy, Marvin. Hypersonic flows as related to the national aerospace plane: Semi-annual research report for the period August 1, 1990 - February 28, 1991. Sunnyvale, Calif: Eloret Institute, 1991.
Den vollen Inhalt der Quelle findenJackson, Thomas L. Shock-turbulence interactions in a reacting flow. Hampton, Va: Institute for Computer Applications in Science and Engineering, 1992.
Den vollen Inhalt der Quelle findenGoldstein, Marvin E. Interaction of oblique instability waves with weak streamwise vortices. [Washington, D.C.]: National Aeronautics and Space Administration, 1994.
Den vollen Inhalt der Quelle findenGoldstein, Marvin E. Interaction of oblique instability waves with weak streamwise vortices. [Washington, D.C.]: National Aeronautics and Space Administration, 1994.
Den vollen Inhalt der Quelle findenRibner, Herbert S. Spectra of noise and amplified turbulence emanating from shock-turbulence interaction. [S.l.]: [s.n.], 1987.
Den vollen Inhalt der Quelle findenG, Briassulis, Langley Research Center und United States. National Aeronautics and Space Administration., Hrsg. Studies of shock wave interactions with homogeneous and isotropic turbulence. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.
Den vollen Inhalt der Quelle findenDunagan, Stephen E. Interferometric data for a shock-wave/boundary-layer interaction. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1986.
Den vollen Inhalt der Quelle findenDunagan, Stephen E. Interferometric data for a shock-wave/boundary-layer interaction. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1986.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration., Hrsg. Spectra of noise and amplified turbulence emanating from shock-turbulence interaction: Two scenarios. [Toronto]: University of Toronto, 1986.
Den vollen Inhalt der Quelle findenD, Saunders J., und United States. National Aeronautics and Space Administration., Hrsg. 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet. [Washington, DC]: National Aeronautics and Space Administration, 1995.
Den vollen Inhalt der Quelle findenD, Saunders J., und United States. National Aeronautics and Space Administration., Hrsg. 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet. [Washington, DC]: National Aeronautics and Space Administration, 1995.
Den vollen Inhalt der Quelle findenD, Saunders J., und United States. National Aeronautics and Space Administration., Hrsg. 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet. [Washington, DC]: National Aeronautics and Space Administration, 1995.
Den vollen Inhalt der Quelle findenD, Saunders J., und United States. National Aeronautics and Space Administration., Hrsg. 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet. [Washington, DC]: National Aeronautics and Space Administration, 1995.
Den vollen Inhalt der Quelle findenC, Horstman K., und Ames Research Center, Hrsg. Intersecting shock-wave/turbulent boundary-layer interactions at Mach 8.3. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1992.
Den vollen Inhalt der Quelle findenC, Horstman K., und Ames Research Center, Hrsg. Intersecting shock-wave/turbulent boundary-layer interactions at Mach 8.3. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1992.
Den vollen Inhalt der Quelle findenC, Horstman K., und Ames Research Center, Hrsg. Intersecting shock-wave/turbulent boundary-layer interactions at Mach 8.3. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1992.
Den vollen Inhalt der Quelle findenC, Horstman K., und Ames Research Center, Hrsg. Intersecting shock-wave/turbulent boundary-layer interactions at Mach 8.3. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1992.
Den vollen Inhalt der Quelle findenR, Hingst W., und United States. National Aeronautics and Space Administration., Hrsg. Surface and flow field measurements in a symmetric crossing shockwave/turbulent boundary-layer interaction. [Washington, DC]: National Aeronautics and Space Administration, 1993.
Den vollen Inhalt der Quelle findenDavis, D. O. Surface and flow field measurements in a symmetric crossing shock wave/turbulent boundary-layer interaction. Cleveland, Ohio: Lewis Research Center, 1992.
Den vollen Inhalt der Quelle findenDélery, J. Turbulent Shear-Layer/Shock-Wave Interactions: IUTAM Symposium, Palaiseau, France September 9-12, 1985. Berlin, Heidelberg: Springer Berlin Heidelberg, 1986.
Den vollen Inhalt der Quelle findenP, Willis B., Hingst W. R und Lewis Research Center, Hrsg. Flowfield measurements in a slot-bled oblique shock wave and turbulent boundary-layer interaction. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.
Den vollen Inhalt der Quelle findenC, Horstman C., und Ames Research Center, Hrsg. Documentation of two- and three-dimensional hypersonic shock wave/turbulent boundary layer interaction flows. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1989.
Den vollen Inhalt der Quelle findenʻAha Hulikoʻa Hawaiian Winter Workshop (4th 1987 University of Hawaii at Manoa). Dynamics of the oceanic surface mixed layer: Proceedings, ʻAha Hulikoʻa Hawaiian Winter Workshop, University of Hawaii at Manoa, January 14-16, 1987. Herausgegeben von Müller Peter 1944-, Henderson Diane, United States. Office of Naval Research., Hawaii Institute of Geophysics und University of Hawaii at Manoa. Dept. of Oceanography. Honolulu: Hawaii Institute of Geophysics, 1987.
Den vollen Inhalt der Quelle findenT, Pot, und United States. National Aeronautics and Space Administration., Hrsg. Shock wave/turbulent boundary layer interaction in the flow field of a tridimensional wind tunnel. Washington D.C: National Aeronautics and Space Administration, 1987.
Den vollen Inhalt der Quelle findenC, Horstman K., und Ames Research Center, Hrsg. Documentation of two- and three-dimensional shock-wave/turbulentboundary-layer interaction flows at Mach 8.2. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1991.
Den vollen Inhalt der Quelle findenA, Ostrovskiĭ L., und Environmental Technology Laboratory (Oceanic and Atmospheric Research Laboratories), Hrsg. Laboratory modeling of interactions between waves and flows in the upper ocean. Boulder, Colo: U.S. Dept. of Commerce, National Oceanic and Atmospheric Administration, Oceanic and Atmospheric Research Laboratories, Environmental Technology Laboratory, 2000.
Den vollen Inhalt der Quelle findenE, Williams Kevin, und United States. National Aeronautics and Space Administration., Hrsg. Interaction of two glancing, crossing shock waves with a turbulent boundary-layer at various Mach numbers. [Washington, DC: National Aeronautics and Space Administration, 1991.
Den vollen Inhalt der Quelle findenCoratekin, Turan. Numerical simulation of turbulent shock/boundary-layer interactions in hypersonic flows. Düsseldorf: VDI Verlag, 2000.
Den vollen Inhalt der Quelle findenHamed, A. Flow separation in shock wave boundary layer interactions at hypersonic speeds. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
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