Książki na temat „Wave turbulence interaction”

Milewski, Paul A., Leslie M. Smith, Fabian Waleffe i Esteban G. Tabak, red. 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., red. 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. i Lewis Research Center. Institute for Computational Mechanics in Propulsion., red. 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. i Symposium on Wave Breaking, Turbulent Mixing and Radio Probing of the Ocean Surface (1984 : Tohoku University), red. 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. Redaktor Milewski Paul A. 1966-. Providence, R.I: American Mathematical Society, 2001.

Center, Langley Research, red. 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, red. 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., i United States. National Aeronautics and Space Administration., red. 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., i United States. National Aeronautics and Space Administration., red. 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., i United States. National Aeronautics and Space Administration., red. 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. Redaktor Shukla P. K. Stockholm: Royal Swedish Academy of Sciences, 1994.

United States. National Aeronautics and Space Administration., red. Turbulence modeling in shock wave/turbulent boundary layer interactions: Final report. [Washington, DC: National Aeronautics and Space Administration, 1992.

Center, Ames Research, red. 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., red. Computational modeling and validation for hypersonic inlets. [Washington, D.C: National Aeronautics and Space Administration, 1990.

Délery, J., red. 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. Redaktorzy Délery J. 1939-, International Union of Theoretical and Applied Mechanics. i 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 i United States. National Aeronautics and Space Administration., red. 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., red. Spectra of noise and amplified turbulence emanating from shock-turbulence interaction: Two scenarios. [Toronto]: University of Toronto, 1986.

D, Saunders J., i United States. National Aeronautics and Space Administration., red. 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., i United States. National Aeronautics and Space Administration., red. 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., i United States. National Aeronautics and Space Administration., red. 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., i United States. National Aeronautics and Space Administration., red. 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., i Ames Research Center, red. 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., i Ames Research Center, red. 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., i Ames Research Center, red. 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., i Ames Research Center, red. 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., i United States. National Aeronautics and Space Administration., red. 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 i Lewis Research Center, red. 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., i Ames Research Center, red. 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. Redaktorzy Müller Peter 1944-, Henderson Diane, United States. Office of Naval Research., Hawaii Institute of Geophysics i University of Hawaii at Manoa. Dept. of Oceanography. Honolulu: Hawaii Institute of Geophysics, 1987.

T, Pot, i United States. National Aeronautics and Space Administration., red. 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., i Ames Research Center, red. 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., i Environmental Technology Laboratory (Oceanic and Atmospheric Research Laboratories), red. 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, i United States. National Aeronautics and Space Administration., red. 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.