Libri sul tema "Turbulent shear layers"

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

Jean-Paul, Dussauge, a cura di. Turbulent shear layers in supersonic flow. 2^a ed. New York: Springer, 2006.

Jean-Paul, Dussauge, a cura di. 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 e Lewis Research Center. Institute for Computational Mechanics in Propulsion., a cura di. 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, a cura di. 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, a cura di. 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 e United States. National Aeronautics and Space Administration., a cura di. Grid resolution and turbulent inflow boundary condition recommendations for NPARC calculations. [Washington, DC]: National Aeronautics and Space Administration, 1995.

F, Durst, e International Symposium on Turbulent Shear Flows, (9th : 1993 : Kyoto, Japan), a cura di. 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., a cura di. 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. A cura di Délery J. 1939-, International Union of Theoretical and Applied Mechanics. e 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., e Langley Research Center, a cura di. 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., a cura di. Turbulence modeling of free shear layers for high performance aircraft. San Jose, CA: MCAT Institute, 1993.

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

United States. National Aeronautics and Space Administration., a cura di. 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. A cura di 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. A cura di Durst F. Berlin: Springer-Verlag, 1993.

L, Bowles Roland, e Langley Research Center, a cura di. 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, e Langley Research Center, a cura di. 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 e United States. National Aeronautics and Space Administration., a cura di. 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., a cura di. 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., a cura di. 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, e United States. National Aeronautics and Space Administration., a cura di. Control of flow separation and mixing by aerodynamic excitation. [Washington, D.C.]: NASA, 1990.

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

C, Yee H., e Research Institute for Advanced Computer Science (U.S.), a cura di. 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., e United States. National Aeronautics and Space Administration., a cura di. 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., e United States. National Aeronautics and Space Administration., a cura di. 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., e United States. National Aeronautics and Space Administration., a cura di. 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., e United States. National Aeronautics and Space Administration., a cura di. Noise from supersonic coaxial jets. [Washington, DC: National Aeronautics and Space Administration, 1997.