Книги з теми "Flow Reynolds number"
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Whalen, Margaret V. Low Reynolds number nozzle flow study. National Aeronautics and Space Administration, 1987.
Знайти повний текст джерелаKohr, Mirela. Viscous incompressible flow for low Reynolds numbers. WIT, 2004.
Знайти повний текст джерелаSandborn, Virgil A. Evaluation of high reynolds number flow in a 180 degree turn-around duct. National Aeronautics and Space Administration, 1991.
Знайти повний текст джерелаJ, Yoo G., and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. On the modeling of low-Reynolds-number turbulence. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.
Знайти повний текст джерелаJ, Yoo G., and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. On the modeling of low-Reynolds-number turbulence. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.
Знайти повний текст джерелаSo, Ronald M. C. On the modeling of low-Reynolds-number turbulence. Lewis Research Center, 1986.
Знайти повний текст джерелаL, Streett Craig, and Langley Research Center, eds. A finite Reynolds number approach for the prediction of boundary layer receptivity in localized regions. National Aeronautics and Space Administration, Langley Research Center, 1991.
Знайти повний текст джерелаChoudhari, Meelan. A finite Reynolds number approach for the prediction of boundary layer receptivity in localized regions. National Aeronautics and Space Administration, Langley Research Center, 1991.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. A finite element computational method for high Reynolds number laminar flows. National Aeronautics and Space Administration, 1987.
Знайти повний текст джерела1940-, Shih Tsan-Hsing, and United States. National Aeronautics and Space Administration., eds. Low Reynolds number two-equation modeling of turbulent flows. NASA, 1991.
Знайти повний текст джерелаLepicovsky, J. Coherent large-scale structures in high Reynolds number supersonic jets. Lockheed-Georgia Company, 1985.
Знайти повний текст джерелаSmits, Alexander J., ed. IUTAM Symposium on Reynolds Number Scaling in Turbulent Flow. Springer Netherlands, 2004. http://dx.doi.org/10.1007/978-94-007-0997-3.
Повний текст джерелаNikas, Konstantinos-Stephen P. Low-Reynolds number computations of flow through rotating cavities. UMIST, 1995.
Знайти повний текст джерелаW, Duck Peter, and Institute for Computer Applications in Science and Engineering., eds. The effects of viscosity on the stability of a trailing-line vortex in compressible flow. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1994.
Знайти повний текст джерелаW, Duck Peter, and Institute for Computer Applications in Science and Engineering., eds. The effects of viscosity on the stability of a trailing-line vortex in compressible flow. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1994.
Знайти повний текст джерелаS, Ukeiley Lawrence, Lee Sang W, and Langley Research Center, eds. Aeroacoustic data for a high Reynolds number axisymmetric subsonic jet. National Aeronautics and Space Administration, Langley Research Center, 1999.
Знайти повний текст джерелаCunningham, Atlee M. A study of the effects of Reynolds number and Mach number on constant pressure coefficient jump for shock-induced trailing-edge separation. Langley Research Center, 1987.
Знайти повний текст джерелаInstitute for Computer Applications in Science and Engineering. and United States. National Aeronautics and Space Administration., eds. Directional agglomeration multigrid techniques for high-Reynolds number viscous flows. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1998.
Знайти повний текст джерелаInstitute for Computer Applications in Science and Engineering., ed. Directional agglomeration multigrid techniques for high-Reynolds number viscous flows. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1998.
Знайти повний текст джерелаDeissler, Robert G. Numerical solution for the velocity-derivative skewness of a low-Reynolds-number decaying Navier-Stokes flow. National Aeronautics and Space Administration, 1990.
Знайти повний текст джерелаMavriplis, Dimitri J. Unstructured and adaptive mesh generation for high Reynolds number viscous flows. Institute for Computer Applications in Science and Engineering, 1991.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Directional agglomeration multigrid techniques for high Reynolds number viscous flow solvers. American Institute of Aeronautics and Astronautics, 1998.
Знайти повний текст джерелаBayliss, Alvin. Wave phenomena in a high Reynolds number compressible boundary layer. ICASE, 1985.
Знайти повний текст джерела1947-, Kim John, Moin Parviz, and Ames Research Center, eds. Reynolds-stress and dissipation rate budgets in a turbulent channel flow. National Aeronautics and Space Administration, Ames Research Center, 1987.
Знайти повний текст джерела1947-, Kim John, Moin Parviz, and Ames Research Center, eds. Reynolds-stress and dissipation rate budgets in a turbulent channel flow. National Aeronautics and Space Administration, Ames Research Center, 1987.
Знайти повний текст джерела1947-, Kim John, Moin Parviz, and Ames Research Center, eds. Reynolds-stress and dissipation rate budgets in a turbulent channel flow. National Aeronautics and Space Administration, Ames Research Center, 1987.
Знайти повний текст джерелаJ, Smits Alexander, ed. IUTAM Symposium on Reynolds Number Scaling in Turbulent Flow: Proceedings of the IUTASM Symposium held in Princeton, NJ, U.S.A., 11-13 September 2002. Kluwer Academic, 2003.
Знайти повний текст джерелаIUTAM Symposium on Reynolds Number Scaling in Turbulent Flow (2002 Princeton, N.J.). IUTAM Symposium on Reynolds Number Scaling in Turbulent Flow: Proceedings of the IUTAM Symposium held in Princeton, NJ, U.S.A., 11-13 September 2002. Kluwer Academic, 2004.
Знайти повний текст джерелаIUTAM Symposium on Reynolds Number Scaling in Turbulent Flow (2002 Princeton, N.J.). IUTAM Symposium on Reynolds Number Scaling in Turbulent Flow: Proceedings of the IUTASM Symposium held in Princeton, NJ, U.S.A., 11-13 September 2002. Kluwer Academic, 2003.
Знайти повний текст джерелаIUTAM Symposium on Reynolds Number Scaling in Turbulent Flow (2002 Princeton, N.J.). IUTAM Symposium on Reynolds Number Scaling in Turbulent Flow: Proceedings of the IUTAM Symposium held in Princeton, NJ, U.S.A., 11-13 September 2002. Springer Science+Business Media, 2004.
Знайти повний текст джерелаIUTAM Symposium on Reynolds Number Scaling in Turbulent Flow (2002 Princeton, N.J.). IUTAM Symposium on Reynolds Number Scaling in Turbulent Flow: Proceedings of the IUTAM symposium held in Princeton, N.J., U.S.A., 11-13 September 2002. Kluwer Academic, 2004.
Знайти повний текст джерелаYuan, S. P. A near-wall Reynolds-stress closure without wall normals. National Aeronautics and Space Administration, 1997.
Знайти повний текст джерелаKeener, Earl R. Flow-separation patterns on symmetric forebodies. Ames Research Center, 1986.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., ed. Flow-separation patterns on symmetric forebodies. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., ed. Flow-separation patterns on symmetric forebodies. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., ed. Flow-separation patterns on symmetric forebodies. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.
Знайти повний текст джерелаZeybek, Birol. Numerical simulation of flow induced by a spinning sphere using spectral methods. Naval Postgraduate School, 1997.
Знайти повний текст джерелаDenier, James P. The three-dimensional flow past a rapidly rotating circular cylinder. Institute for Computer Applications in Science and Engineering, 1993.
Знайти повний текст джерелаW, Duck Peter, and Langley Research Center, eds. The three-dimensional flow past a rapidly rotating circular cylinder. National Aeronautics and Space Administration, Langley Research Center, 1993.
Знайти повний текст джерелаW, Duck Peter, and Langley Research Center, eds. The three-dimensional flow past a rapidly rotating circular cylinder. National Aeronautics and Space Administration, Langley Research Center, 1993.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. NASA Dryden Flow Visualization Facility. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1995.
Знайти повний текст джерелаMa, King Lok Kenneth. Low Reynolds number flow in the presence of a corrugated boundary. [s.n.], 1994.
Знайти повний текст джерелаBinek, Alexander P. A study of the aerodynamic effect of an obstacle attached to the leeward side of a sphere in low-speed flow. University of Toronto, Institute for Aerospace Studies, 2002.
Знайти повний текст джерелаJ, Donnelly Russell, and Sreenivasan Katepalli R, eds. Flow at ultra-high Reynolds and Rayleigh numbers: A status report. Springer, 1998.
Знайти повний текст джерелаC, So Ronald M., and United States. National Aeronautics and Space Administration., eds. A near-wall Reynolds-stress closure without wall normals: Final report ... under grant number NAG-1-1772. College of Engineering and Applied Sciences, Arizona State University, 1997.
Знайти повний текст джерелаC, So Ronald M., and United States. National Aeronautics and Space Administration., eds. A near-wall Reynolds-stress closure without wall normals: Final report ... under grant number NAG-1-1772. College of Engineering and Applied Sciences, Arizona State University, 1997.
Знайти повний текст джерелаC, So Ronald M., and United States. National Aeronautics and Space Administration., eds. A near-wall Reynolds-stress closure without wall normals: Final report ... under grant number NAG-1-1772. College of Engineering and Applied Sciences, Arizona State University, 1997.
Знайти повний текст джерелаC, So Ronald M., and United States. National Aeronautics and Space Administration., eds. A near-wall Reynolds-stress closure without wall normals: Final report ... under grant number NAG-1-1772. College of Engineering and Applied Sciences, Arizona State University, 1997.
Знайти повний текст джерелаHicks, R. M. An evaluation of three two-dimensional computational fluid dynamics codes including low Reynolds numbers and transonic Mach numbers. Ames Research Center, 1991.
Знайти повний текст джерела