Books on the topic '(e/D); Flow Reynolds number'
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Whalen, Margaret V. Low Reynolds number nozzle flow study. National Aeronautics and Space Administration, 1987.
Find full text1940-, Shih Tsan-Hsing, and United States. National Aeronautics and Space Administration., eds. Low Reynolds number two-equation modeling of turbulent flows. NASA, 1991.
Find full textSandborn, Virgil A. Evaluation of high reynolds number flow in a 180 degree turn-around duct. National Aeronautics and Space Administration, 1991.
Find full textJ, 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.
Find full textJ, 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.
Find full textSo, Ronald M. C. On the modeling of low-Reynolds-number turbulence. Lewis Research Center, 1986.
Find full textSmits, 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.
Full textNikas, Konstantinos-Stephen P. Low-Reynolds number computations of flow through rotating cavities. UMIST, 1995.
Find full textLepicovsky, J. Coherent large-scale structures in high Reynolds number supersonic jets. Lockheed-Georgia Company, 1985.
Find full textL, 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.
Find full textChoudhari, 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.
Find full textUnited States. National Aeronautics and Space Administration., ed. A finite element computational method for high Reynolds number laminar flows. National Aeronautics and Space Administration, 1987.
Find full textS, 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.
Find full textInstitute 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.
Find full textInstitute 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.
Find full textMavriplis, Dimitri J. Unstructured and adaptive mesh generation for high Reynolds number viscous flows. Institute for Computer Applications in Science and Engineering, 1991.
Find full textBayliss, Alvin. Wave phenomena in a high Reynolds number compressible boundary layer. ICASE, 1985.
Find full textMa, King Lok Kenneth. Low Reynolds number flow in the presence of a corrugated boundary. [s.n.], 1994.
Find full textUnited 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.
Find full textW, 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.
Find full textW, 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.
Find full textYuan, S. P. A near-wall Reynolds-stress closure without wall normals. National Aeronautics and Space Administration, 1997.
Find full textCunningham, 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.
Find full textDeissler, Robert G. Numerical solution for the velocity-derivative skewness of a low-Reynolds-number decaying Navier-Stokes flow. National Aeronautics and Space Administration, 1990.
Find full textKeener, Earl R. Flow-separation patterns on symmetric forebodies. Ames Research Center, 1986.
Find full textUnited 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.
Find full textUnited 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.
Find full textUnited 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.
Find full text1947-, 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.
Find full text1947-, 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.
Find full text1947-, 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.
Find full textJ, Donnelly Russell, and Sreenivasan Katepalli R, eds. Flow at ultra-high Reynolds and Rayleigh numbers: A status report. Springer, 1998.
Find full textUnited 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.
Find full textJ, 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.
Find full textIUTAM 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.
Find full textIUTAM 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.
Find full textIUTAM 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.
Find full textIUTAM 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.
Find full textZeybek, Birol. Numerical simulation of flow induced by a spinning sphere using spectral methods. Naval Postgraduate School, 1997.
Find full textDenier, James P. The three-dimensional flow past a rapidly rotating circular cylinder. Institute for Computer Applications in Science and Engineering, 1993.
Find full textW, 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.
Find full textW, 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.
Find full textFossen, G. James Van. Influence of turbulence parameters, Reynolds number, and body shape on stagnation-region heat transfer. Lewis Research Center, 1994.
Find full textJ, Simoneau Robert, Ching Chang Y, and United States. National Aeronautics and Space Administration., eds. Influence of turbulence parameters, Reynolds number, and body shape on stagnation-region heat transfer. National Aeronautics and Space Administration, 1994.
Find full textC, 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.
Find full textC, 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.
Find full textC, 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.
Find full textC, 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.
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