Książki na temat „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.
Znajdź pełny tekst źródłaJ, 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.
Znajdź pełny tekst źródłaSo, Ronald M. C. On the modeling of low-Reynolds-number turbulence. Lewis Research Center, 1986.
Znajdź pełny tekst źródłaCenter, Langley Research, ed. Unstructured and adaptive mesh generation for high Reynolds number viscous flows. National Aeronautics and Space Administration, Langley Research Center, 1991.
Znajdź pełny tekst źródłaJoseph, Katz. Final report for the grant integration of viscous effects into inviscid computational methods. National Aeronautics and Space Administration, 1990.
Znajdź pełny tekst źródłaSandborn, Virgil A. Evaluation of high reynolds number flow in a 180 degree turn-around duct. National Aeronautics and Space Administration, 1991.
Znajdź pełny tekst źródłaJoseph, Katz. Final report for the grant integration of viscous effects into inviscid computational methods. National Aeronautics and Space Administration, 1990.
Znajdź pełny tekst źródłaUnited 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.
Znajdź pełny tekst źródłaMueller, Thomas J., ed. Low Reynolds Number Aerodynamics. Springer Berlin Heidelberg, 1989. http://dx.doi.org/10.1007/978-3-642-84010-4.
Pełny tekst źródłaMorgan, 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.
Znajdź pełny tekst źródłaThomas, 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.
Znajdź pełny tekst źródłaWalker, J. D. A. Wall-layer eruptions in turbulent flows. National Aeronautics and Space Administration, 1990.
Znajdź pełny tekst źródłaWalker, J. D. A. Wall-layer eruptions in turbulent flows. National Aeronautics and Space Administration, 1990.
Znajdź pełny tekst źródłaMorgan, 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.
Znajdź pełny tekst źródłaMorgan, 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.
Znajdź pełny tekst źródłaWalker, J. D. A. Wall-layer eruptions in turbulent flows. National Aeronautics and Space Administration, 1990.
Znajdź pełny tekst źródłaM, Bushnell Dennis, and Langley Research Center, eds. Reynolds number influences in aeronautics. National Aeronautics and Space Administration, Langley Research Center, 1993.
Znajdź pełny tekst źródłaJ, 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.
Znajdź pełny tekst źródłaIUTAM 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.
Znajdź pełny tekst źródłaIUTAM 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.
Znajdź pełny tekst źródłaKuhn, Gary D. Investigation of the validity of Reynolds averaged turbulence models at the frequencies that occur in turbomachinery. National Aeronautics and Space Administration, 1988.
Znajdź pełny tekst źródłaM, 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.
Znajdź pełny tekst źródłaUnited 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.
Znajdź pełny tekst źródłaS, 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.
Znajdź pełny tekst źródłaM, 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.
Znajdź pełny tekst źródłaL, 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.
Znajdź pełny tekst źródłaIUTAM 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.
Znajdź pełny tekst źródłaM, 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.
Znajdź pełny tekst źródłaUnited 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.
Znajdź pełny tekst źródłaChoudhari, 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.
Znajdź pełny tekst źródłaUnited States. National Aeronautics and Space Administration., ed. A finite element computational method for high Reynolds number laminar flows. National Aeronautics and Space Administration, 1987.
Znajdź pełny tekst źródłaPenland, 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.
Znajdź pełny tekst źródłaIUTAM 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.
Znajdź pełny tekst źródłaKohr, Mirela. Viscous incompressible flow for low Reynolds numbers. WIT, 2004.
Znajdź pełny tekst źródłaCunningham, 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.
Znajdź pełny tekst źródłaWhalen, Margaret V. Low Reynolds number nozzle flow study. National Aeronautics and Space Administration, 1987.
Znajdź pełny tekst źródłaBodnar, Andrea Claire. Low Reynolds number particle-fluid interactions. [s.n.], 1994.
Znajdź pełny tekst źródłaGeorge 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.
Znajdź pełny tekst źródłaA, 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.
Znajdź pełny tekst źródłaGrosche, Friedrich R. Windkanaluntersuchungen mit akustischen Messmethoden zur periodischen Stromungsablosung an Kreiszylindern mit rauher Oberflache. DFVLR, 1987.
Znajdź pełny tekst źródłaJohnson, 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.
Znajdź pełny tekst źródłaKhalid, M. Further studies on the 21% thick, supercritical NLR airfoil NAE 68-060-21:1. National Aeronautical Establishment, 1986.
Znajdź pełny tekst źródłaDeissler, Robert G. Numerical solution for the velocity-derivative skewness of a low-Reynolds-number decaying Navier-Stokes flow. National Aeronautics and Space Administration, 1990.
Znajdź pełny tekst źródłaPitts, 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.
Znajdź pełny tekst źródłaUnited 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.
Znajdź pełny tekst źródłaBinek, 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.
Znajdź pełny tekst źródłaGeorge 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.
Znajdź pełny tekst źródłaHeiko, Schmitt, ed. Flows at large reynolds numbers. Computational Mechanics Pub., 1997.
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