Books on the topic 'Reynolds's number'
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J, 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 textCenter, Langley Research, ed. Unstructured and adaptive mesh generation for high Reynolds number viscous flows. National Aeronautics and Space Administration, Langley Research Center, 1991.
Find full textJoseph, Katz. Final report for the grant integration of viscous effects into inviscid computational methods. National Aeronautics and Space Administration, 1990.
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 textJoseph, Katz. Final report for the grant integration of viscous effects into inviscid computational methods. National Aeronautics and Space Administration, 1990.
Find full textUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. Effects of independent variation of Mach and Reynolds numbers on the low-speed aerodynamic characteristics of the NACA 0012 airfoil section. National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
Find full textMueller, Thomas J., ed. Low Reynolds Number Aerodynamics. Springer Berlin Heidelberg, 1989. http://dx.doi.org/10.1007/978-3-642-84010-4.
Full textMorgan, Harry L. A study of high-lift airfoils at high Reynolds numbers in the Langley Low-Turbulence Pressure Tunnel. National Aeronautics and Space Administration, Scientific and Technical Information Office, 1989.
Find full textThomas, Stengle, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Flight Mechanics/Estimation Theory Symposium, 1989: Proceedings of a symposium sponsored by NASA Goddard Space Flight Center and held at Goddard Space Flight Center, Greenbelt, Maryland, May 23-24, 1989. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.
Find full textWalker, J. D. A. Wall-layer eruptions in turbulent flows. National Aeronautics and Space Administration, 1990.
Find full textWalker, J. D. A. Wall-layer eruptions in turbulent flows. National Aeronautics and Space Administration, 1990.
Find full textMorgan, Harry L. A study of high-lift airfoils at high Reynolds numbers in the Langley Low-Turbulence Pressure Tunnel. National Aeronautics and Space Administration, Scientific and Technical Information Office, 1989.
Find full textMorgan, Harry L. A study of high-lift airfoils at high Reynolds numbers in the Langley Low-Turbulence Pressure Tunnel. National Aeronautics and Space Administration, Scientific and Technical Information Office, 1989.
Find full textWalker, J. D. A. Wall-layer eruptions in turbulent flows. National Aeronautics and Space Administration, 1990.
Find full textM, Bushnell Dennis, and Langley Research Center, eds. Reynolds number influences in aeronautics. National Aeronautics and Space Administration, Langley Research Center, 1993.
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 textKuhn, Gary D. Investigation of the validity of Reynolds averaged turbulence models at the frequencies that occur in turbomachinery. National Aeronautics and Space Administration, 1988.
Find full textM, Russell Louis, and United States. National Aeronautics and Space Administration., eds. High-resolution liquid crystal heat transfer measurements on the end wall of a turbine passage with variations in Reynolds number. National Aeronautics and Space Administration, 1989.
Find full textUnited States. National Aeronautics and Space Administration., ed. Fast methods to numerically integrate the Reynolds equation for gas fluid films. National Aeronautics and Space Administration, 1992.
Find full textS, Hill Aquilla, Ray Edward J, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Aerodynamic performance and pressure distributions for a NASA SC(2)-0714 airfoil tested in the Langley 0.3-meter Transonic Cryogenic Tunnel. National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
Find full textM, Russell Louis, and United States. National Aeronautics and Space Administration., eds. High-resolution liquid crystal heat transfer measurements on the end wall of a turbine passage with variations in Reynolds number. National Aeronautics and Space Administration, 1989.
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 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 textM, Russell Louis, and United States. National Aeronautics and Space Administration., eds. High-resolution liquid crystal heat transfer measurements on the end wall of a turbine passage with variations in Reynolds number. National Aeronautics and Space Administration, 1989.
Find full textUnited States. National Aeronautics and Space Administration., ed. Comment on "Local energy transfer and nonlocal interactions in homogeneous, isotropic turbulence" [Phys. Fluids A2, 413 (1990)]. National Aeronautics and Space Administration, 1990.
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 textPenland, Jim A. Effect of Reynolds number variation on aerodynamics of a hydrogen-fueled transport concept at Mach 6. National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.
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 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 textWhalen, Margaret V. Low Reynolds number nozzle flow study. National Aeronautics and Space Administration, 1987.
Find full textBodnar, Andrea Claire. Low Reynolds number particle-fluid interactions. [s.n.], 1994.
Find full textGeorge C. Marshall Space Flight Center., ed. Velocity-pressure integrated versus penalty finite element methods for high Reynolds number flows. NASA-Marshall Space Flight Center, 1988.
Find full textA, Kilgore Robert, McGuire Peggy D, and Langley Research Center, eds. Cryogenic wind tunnels for high Reynolds number testing. v National Aeronautics and Space Adminisatration, Langley Research Center, 1986.
Find full textGrosche, Friedrich R. Windkanaluntersuchungen mit akustischen Messmethoden zur periodischen Stromungsablosung an Kreiszylindern mit rauher Oberflache. DFVLR, 1987.
Find full textJohnson, William G. High Reynolds number tests of a NASA SC(3)-0712(b) airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnels. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
Find full textKhalid, M. Further studies on the 21% thick, supercritical NLR airfoil NAE 68-060-21:1. National Aeronautical Establishment, 1986.
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 textPitts, William M. Effects of global density and Reynolds number variations on mixing in turbulent, axisymmetric jets. U.S. Dept. of Commerce, National Bureau of Standards, 1986.
Find full textUnited States. National Aeronautics and Space Administration., ed. An efficient and robust algorithm for two dimensional time dependent incompressible Navier-Stokes equations: High Reynolds number flows. National Aeronautics and Space Administration, 1991.
Find full textBinek, 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.
Find full textGeorge C. Marshall Space Flight Center., ed. Velocity-pressure integrated versus penalty finite element methods for high Reynolds number flows. NASA-Marshall Space Flight Center, 1988.
Find full textHeiko, Schmitt, ed. Flows at large reynolds numbers. Computational Mechanics Pub., 1997.
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