Книги з теми "Turbulent shear layers"

Smits, Alexander J. Turbulent shear layers in supersonic flow. 2nd ed. New York: Springer, 2011.

Jean-Paul, Dussauge, ed. Turbulent shear layers in supersonic flow. 2nd ed. New York: Springer, 2006.

Jean-Paul, Dussauge, ed. Turbulent shear layers in supersonic flow. Woodbury, N.Y: American Institute of Physics, 1996.

Papamoschou, Dimitri. Structure of the compressible turbulent shear layer. Washington, D. C: American Institute of Aeronautics and Astronautics, 1989.

Y, Chen J., Limley J. L, and Lewis Research Center. Institute for Computational Mechanics in Propulsion., eds. Second order modeling of boundary-free turbulent shear flows. Cleveland, Ohio: NASA Lewis Research Center, Institute for Computational Mechanics in Propulsion, 1991.

Shau, Y. R. Experimental study of spreading rate enhancement of high Mach number turbulent shear layers. Washington, D. C: American Institute of Aeronautics and Astronautics, 1989.

Center, Ames Research, ed. Improved two-equation k - [omega] turbulence models for aerodynamic flows. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1992.

Center, Ames Research, ed. Improved two-equation k - [omega] turbulence models for aerodynamic flows. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1992.

Adair, Desmond. Characteristics of merging shear layers and turbulent wakes of a multi-element airfoil. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1988.

Brown, Douglas L. Computation of turbulent boundary layers employing the defect wall-function method. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

C, Dudek Julianne, Tierney Thomas P, and United States. National Aeronautics and Space Administration., eds. Grid resolution and turbulent inflow boundary condition recommendations for NPARC calculations. [Washington, DC]: National Aeronautics and Space Administration, 1995.

F, Durst, and International Symposium on Turbulent Shear Flows, (9th : 1993 : Kyoto, Japan), eds. Turbulent shear flows 9: Selected papers from the Ninth International Symposium on Turbulent Shear Flows, Kyoto, Japan, August 16-18, 1993. Berlin: Springer-Verlag, 1995.

University), International Symposium on Turbulent Shear Flows (7th 1989 Stanford. Turbulent shear flows 7: Selected papers from the Seventh International Symposium on Turbulent Shear Flows, Stanford University, USA, August 21-23, 1989. Berlin: Springer-Verlag, 1991.

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.

International Symposium on Turbulent Shear Flows (5th 1985 Cornell University, Ithaca, N.Y.). Turbulent shear flows: Papers from the Fifth International Symposium on Turbulent Shear Flows, August 7-9, 1985, Cornell University, Ithaca, NY. [University Park, Pa: Pennsylvania State University, 1985.

Woppowa, Stefan. Über Gedächtniseffekte in der Turbulenz. Köln: Deutsche Forschungsanstalt für Luft- und Raumfahrt, 1993.

American Society of Mechanical Engineers. Winter Meeting. Shear flow: Structure interaction phenomena. New York, N.Y. (345 E. 47th St., New York): American Society of Mechanical Engineers, 1985.

Kim, S. W. Calculation of reattaching shear layers in divergent channel with a multiple-time-scale turbulence model. Cleveland, Ohio: Institute for Computational Mechanics in Propulusion, 1989.

B, Gatski T., and Langley Research Center, eds. An alternative assessment of second order closure models in turbulent shear flows. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1994.

Driver, David M. Experimental study of a three-dimensional shear-driven turbulent boundary layer with streamwise adverse pressure gradient. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1990.

United States. National Aeronautics and Space Administration., ed. Turbulence modeling of free shear layers for high performance aircraft. San Jose, CA: MCAT Institute, 1993.

United States. National Aeronautics and Space Administration., ed. Turbulence modeling of free shear layers for high performance aircraft. San Jose, CA: MCAT Institute, 1993.

United States. National Aeronautics and Space Administration., ed. Turbulence modeling of free shear layers for high-performance aircraft. San Jose, CA: MCAT Institute, 1993.

International Symposium on Turbulent Shear Flows (9th 1993 Kyoto, Japan). Turbulent shear flows 9: Selected papers from the Ninth International Symposium on Turbulent Shear Flows, Kyoto, Japan, August 16-18, 1993. Edited by Durst F. Berlin: Springer-Verlag, 1995.

International Symposium on Turbulent Shear Flows (8th 1991 Munich, Germany). Turbulent shear flows 8: Selected papers from the Eighth International Symposium on Turbulent Shear Flows, Munich, FRG, September 9-11, 1991. Edited by Durst F. Berlin: Springer-Verlag, 1993.

L, Bowles Roland, and Langley Research Center, eds. A simple, analytic 3-dimensional downburst model based on boundary layer stagnation flow. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.

L, Bowles Roland, and Langley Research Center, eds. A simple, analytic 3-dimensional downburst model based on boundary layer stagnation flow. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.

G, Huang P., MacInnes J. M, and United States. National Aeronautics and Space Administration., eds. Mesh refinement in a two-dimensional large eddy simulation of a forced shear layer. [Washington, DC]: National Aeronautics and Space Administration, 1989.

Sarkar, Sutanu. Application of a Reynolds stress turbulence model to the compressible shear layer. Hampton, Va: Institute for Computer Applications in Science and Engineering, 1990.

Driver, David M. Experimental study of a three-dimensional, shear-driven, turbulent boundary layer using a three-dimensional laser doppler velocimeter. [New York]: American Institute of Aeronautics and Astronautics, 1985.

Délery, J. Turbulent Shear-Layer/Shock-Wave Interactions: IUTAM Symposium, Palaiseau, France September 9-12, 1985. Berlin, Heidelberg: Springer Berlin Heidelberg, 1986.

Sarkar, Sarben. Application of a Reynolds stress turbulence model to the compressible shear layer. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

IUTAM Symposium (1993 Potsdam, N.Y.). Nonlinear instability of nonparallel flows. Berlin: Springer-Verlag, 1994.

United States. National Aeronautics and Space Administration., ed. Low re multiple-time-scale turbulence model and calculations of steady and pulsating shear layers. [Washington, DC]: National Aeronautics and Space Administration, 1992.

United States. National Aeronautics and Space Administration., ed. Low re multiple-time-scale turbulence model and calculations of steady and pulsating shear layers. [Washington, DC]: National Aeronautics and Space Administration, 1992.

M, Abbott John, and United States. National Aeronautics and Space Administration., eds. Control of flow separation and mixing by aerodynamic excitation. [Washington, D.C.]: NASA, 1990.

M, Abbott John, and United States. National Aeronautics and Space Administration., eds. Control of flow separation and mixing by aerodynamic excitation. [Washington, D.C.]: NASA, 1990.

C, Yee H., and Research Institute for Advanced Computer Science (U.S.), eds. Performance of low dissipative high order shock-capturing schemes for shock-turbulence interactions. [Moffett Field, Calif.]: Research Institute for Advanced Computer Science, NASA Ames Research Center, 1998.

Kline, Stephen. The physics of turbulence in the boundary layer: Final report ... NASA grant NAG-1-1610. [Washington, DC: National Aeronautics and Space Administration, 1996.

Clawson, K. L. Meteorological measurements during the urban 2000/VTMX field study. Silver Spring, Md: U.S. Dept. of Commerce, National Oceanic and Atmospheric Administration, Oceanic and Atmospheric Research Laboratories, Air Resources Laboratory, 2002.

T, Chang C., and United States. National Aeronautics and Space Administration., eds. Turbulence measurement in a reacting and non-reacting shear layer at a high subsonic Mach number. [Washington, DC]: National Aeronautics and Space Administration, 1993.

T, Chang C., and United States. National Aeronautics and Space Administration., eds. Turbulence measurement in a reacting and non-reacting shear layer at a high subsonic Mach number. [Washington, DC]: National Aeronautics and Space Administration, 1993.

Kamada, Ray. Amending the w* velocity scale for surface layer, entrainment zone, and baroclinic shear in mixed forced/free turbulent convection. Monterey, Calif: Naval Postgraduate School, 1992.

Dahl, M. D. Noise from supersonic coaxial jets. [Washington, DC: National Aeronautics and Space Administration, 1997.

Dahl, M. D. Noise from supersonic coaxial jets. [Washington, DC: National Aeronautics and Space Administration, 1997.

J, Morris P., and United States. National Aeronautics and Space Administration., eds. Noise from supersonic coaxial jets. [Washington, DC: National Aeronautics and Space Administration, 1997.

Dahl, M. D. Noise from supersonic coaxial jets. [Washington, DC: National Aeronautics and Space Administration, 1997.

Dahl, M. D. Noise from supersonic coaxial jets. [Washington, DC: National Aeronautics and Space Administration, 1997.

J, Morris P., and United States. National Aeronautics and Space Administration., eds. Noise from supersonic coaxial jets. [Washington, DC: National Aeronautics and Space Administration, 1997.