Книги з теми "Wave turbulence interaction"
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Milewski, Paul A., Leslie M. Smith, Fabian Waleffe, and Esteban G. Tabak, eds. Advances in Wave Interaction and Turbulence. Providence, Rhode Island: American Mathematical Society, 2001. http://dx.doi.org/10.1090/conm/283.
Lee, Sangsan. Interaction of isotropic turbulence with a shock wave. Stanford, Calif: Thermo sciences Division, Dept. of Mechanical Engineering, Stanford University, 1992.
Ribner, Herbert S. Spectrum of noise from shock-turbulence interaction. [S.l.]: [s.n.], 1986.
United States. National Aeronautics and Space Administration., ed. A simple theory of capillary-gravity wave turbulence. [Washington, DC: National Aeronautics and Space Administration, 1995.
Rubinstein, Robert. The dissipation range in rotating turbulence. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1999.
Kim, 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.
United States. National Aeronautics and Space Administration. and Lewis Research Center. Institute for Computational Mechanics in Propulsion., eds. Numerical investigation of separated transonic turbulent flows with a multiple-time-scale turbulence model. [Washington, D.C: National Aeronautics and Space Administration, 1990.
1931-, Toba Y., Mitsuyasu Hisashi 1929-, IOC/SCOR Committee on Climatic Changes and the Ocean., WMO/ICSU Joint Scientific Committee., and Symposium on Wave Breaking, Turbulent Mixing and Radio Probing of the Ocean Surface (1984 : Tohoku University), eds. The Ocean surface: Wave breaking, turbulent mixing, and radio probing. Dordrecht [Netherlands]: Reidel, 1985.
AMS-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. Edited by Milewski Paul A. 1966-. Providence, R.I: American Mathematical Society, 2001.
Center, Langley Research, ed. 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.
Center, Langley Research, ed. 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.
K, Wideman J., and United States. National Aeronautics and Space Administration., eds. 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.
K, Wideman J., and United States. National Aeronautics and Space Administration., eds. 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.
K, Wideman J., and United States. National Aeronautics and Space Administration., eds. 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.
Spring 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. Edited by Shukla P. K. Stockholm: Royal Swedish Academy of Sciences, 1994.
United States. National Aeronautics and Space Administration., ed. Turbulence modeling in shock wave/turbulent boundary layer interactions: Final report. [Washington, DC: National Aeronautics and Space Administration, 1992.
Center, Ames Research, ed. Turbulence modeling for sharp-fin-induced shock wave/turbulent boundary-layer interactions. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1990.
United States. National Aeronautics and Space Administration., ed. Computational modeling and validation for hypersonic inlets. [Washington, D.C: National Aeronautics and Space Administration, 1990.
Délery, J., ed. Turbulent Shear-Layer/Shock-Wave Interactions. Berlin, Heidelberg: Springer Berlin Heidelberg, 1986. http://dx.doi.org/10.1007/978-3-642-82770-9.
IUTAM Symposium (1985 Palaiseau, France). Turbulent shear-layer/shock-wave interactions. Edited by Délery J. 1939-, International Union of Theoretical and Applied Mechanics., and France. Office national d'études et de recherches aérospatiales. Berlin: Springer-Verlag, 1986.
Mankbadi, Reda R. Multiwave interactions in turbulent jets. Cleveland, Ohio: Institute for Computational Mechanics in Propulsion, 1989.
Kussoy, 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.
Jackson, Thomas L. Shock-turbulence interactions in a reacting flow. Hampton, Va: Institute for Computer Applications in Science and Engineering, 1992.
Goldstein, Marvin E. Interaction of oblique instability waves with weak streamwise vortices. [Washington, D.C.]: National Aeronautics and Space Administration, 1994.
Goldstein, Marvin E. Interaction of oblique instability waves with weak streamwise vortices. [Washington, D.C.]: National Aeronautics and Space Administration, 1994.
Ribner, Herbert S. Spectra of noise and amplified turbulence emanating from shock-turbulence interaction. [S.l.]: [s.n.], 1987.
G, Briassulis, Langley Research Center, and United States. National Aeronautics and Space Administration., eds. Studies of shock wave interactions with homogeneous and isotropic turbulence. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.
Dunagan, Stephen E. Interferometric data for a shock-wave/boundary-layer interaction. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1986.
Dunagan, Stephen E. Interferometric data for a shock-wave/boundary-layer interaction. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1986.
United States. National Aeronautics and Space Administration., ed. Spectra of noise and amplified turbulence emanating from shock-turbulence interaction: Two scenarios. [Toronto]: University of Toronto, 1986.
D, Saunders J., and United States. National Aeronautics and Space Administration., eds. 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet. [Washington, DC]: National Aeronautics and Space Administration, 1995.
D, Saunders J., and United States. National Aeronautics and Space Administration., eds. 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet. [Washington, DC]: National Aeronautics and Space Administration, 1995.
D, Saunders J., and United States. National Aeronautics and Space Administration., eds. 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet. [Washington, DC]: National Aeronautics and Space Administration, 1995.
D, Saunders J., and United States. National Aeronautics and Space Administration., eds. 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet. [Washington, DC]: National Aeronautics and Space Administration, 1995.
C, Horstman K., and Ames Research Center, eds. Intersecting shock-wave/turbulent boundary-layer interactions at Mach 8.3. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1992.
C, Horstman K., and Ames Research Center, eds. Intersecting shock-wave/turbulent boundary-layer interactions at Mach 8.3. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1992.
C, Horstman K., and Ames Research Center, eds. Intersecting shock-wave/turbulent boundary-layer interactions at Mach 8.3. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1992.
C, Horstman K., and Ames Research Center, eds. Intersecting shock-wave/turbulent boundary-layer interactions at Mach 8.3. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1992.
R, Hingst W., and United States. National Aeronautics and Space Administration., eds. Surface and flow field measurements in a symmetric crossing shockwave/turbulent boundary-layer interaction. [Washington, DC]: National Aeronautics and Space Administration, 1993.
Davis, D. O. Surface and flow field measurements in a symmetric crossing shock wave/turbulent boundary-layer interaction. Cleveland, Ohio: Lewis Research Center, 1992.
Délery, J. Turbulent Shear-Layer/Shock-Wave Interactions: IUTAM Symposium, Palaiseau, France September 9-12, 1985. Berlin, Heidelberg: Springer Berlin Heidelberg, 1986.
P, Willis B., Hingst W. R, and Lewis Research Center, eds. 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.
C, Horstman C., and Ames Research Center, eds. 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.
ʻAha 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. Редактори Müller Peter 1944-, Henderson Diane, United States. Office of Naval Research., Hawaii Institute of Geophysics та University of Hawaii at Manoa. Dept. of Oceanography. Honolulu: Hawaii Institute of Geophysics, 1987.
T, Pot, and United States. National Aeronautics and Space Administration., eds. Shock wave/turbulent boundary layer interaction in the flow field of a tridimensional wind tunnel. Washington D.C: National Aeronautics and Space Administration, 1987.
C, Horstman K., and Ames Research Center, eds. 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.
A, Ostrovskiĭ L., and Environmental Technology Laboratory (Oceanic and Atmospheric Research Laboratories), eds. 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.
E, Williams Kevin, and United States. National Aeronautics and Space Administration., eds. Interaction of two glancing, crossing shock waves with a turbulent boundary-layer at various Mach numbers. [Washington, DC: National Aeronautics and Space Administration, 1991.
Coratekin, Turan. Numerical simulation of turbulent shock/boundary-layer interactions in hypersonic flows. Düsseldorf: VDI Verlag, 2000.
Hamed, 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.