Libros sobre el tema "Flow gradients"

E, Zorumski W., Rawls John W y Langley Research Center, eds. Experimental feasibility of investigating acoustic waves in Couette flow with entropy and pressure gradients. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

Otto, S. R. The effect of crossflow on Görtler vortices. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1994.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., ed. A root-mean-square pressure fluctuations model for internal flow applications. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

P, Leonard B. y United States. National Aeronautics and Space Administration., eds. A modified mixing length turbulence model for zero and adverse pressure gradients. [Washington, DC]: National Aeronautics and Space Administration, 1994.

Conley, J. M. A modified mixing length turbulence model for zero and adverse pressure gradients. [Washington, DC]: National Aeronautics and Space Administration, 1994.

Johnston, Craig M. Documentation and application of a method to compute maximum slope and aspect of hydraulic gradients. Pembroke, N.H: U.S. Dept. of the Interior, U.S. Geological Survey, 1998.

Johnston, Craig M. Documentation and application of a method to compute maximum slope and aspect of hydraulic gradients. Pembroke, N.H: U.S. Dept. of the Interior, U.S. Geological Survey, 1998.

Johnston, Craig M. Documentation and application of a method to compute maximum slope and aspect of hydraulic gradients. Pembroke, N.H: U.S. Dept. of the Interior, U.S. Geological Survey, 1998.

E, Kelly R. y United States. National Aeronautics and Space Administration., eds. Effect of density gradients in confined supersonic shear layers. [Washington, DC: National Aeronautics and Space Administration, 1994.

Li, C. Mixing enhancement due to pressure and density gradients generated by expansion waves in supersonic flows. Washington, D. C: American Institute of Aeronautics and Astronautics, 1991.

M, Kassir S., Larwood S. M y United States. National Aeronautics and Space Administration., eds. The influence of free-stream turbulence on turbulent boundary layers with mild adverse pressure gradients: Final report, NASA Cooperative Agreement NCC2-450 covering the period January, 1987-January 1989. San Luis Obispo, Calif: Aeronautical Engineering Dept., California Polytechnic State University ; [Washington, D.C., 1988.

United States. National Aeronautics and Space Administration., ed. Summary of work on shock wave feature extraction in 3-D datasets. [Washington, DC: National Aeronautics and Space Administration, 1996.

Center, Ames Research, ed. 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, ed. Improved two-equation k - [omega] turbulence models for aerodynamic flows. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1992.

Zingg, D. W. Higher-order approximations in interactive airfoil calculations. [Downsview, Ont.]: University of Toronto, 1987.

United States. National Aeronautics and Space Administration., ed. Transitional boundary layers under the influence of high free stream turbulence, intensive wall cooling and high pressure gradinets in hot gas circulation. Washington, D. C: National Aeronautics and Space Administration, 1987.

Zingg, D. W. Higher-order approximations in interactive airfoil calculations. [Downsview, Ont.]: Institute for Aerospace Studies, 1988.

Center, Langley Research, ed. Swept-wing receptivity studies using distributed roughness: Annual technical report. Tempe, AZ: Mechanical and Aerospace Engineering, College of Engineering and Applied Science, Arizona State University, 1998.

Center, Langley Research, ed. Swept-wing receptivity studies using distributed roughness: Annual technical report. Tempe, AZ: Mechanical and Aerospace Engineering, College of Engineering and Applied Science, Arizona State University, 1998.

Center, Langley Research, ed. Swept-wing receptivity studies using distributed roughness: Annual technical report. Tempe, AZ: Mechanical and Aerospace Engineering, College of Engineering and Applied Science, Arizona State University, 1998.

Center, Langley Research, ed. Swept-wing receptivity studies using distributed roughness: Annual technical report. Tempe, AZ: Mechanical and Aerospace Engineering, College of Engineering and Applied Science, Arizona State University, 1998.

United States. National Aeronautics and Space Administration., ed. Experimental and theoretical studies of capillary-pumped loop heat pipes: Progress report for period January 15, 1994-July 15, 1994. Potsdam, N.Y: Clarkson University, 1994.

1929-, Chung T. J. y United States. National Aeronautics and Space Administration., eds. Flowfield-dependent mixed explicit-implicit (FDMEI) algorithm for computational fluid dynamics: Final report ... [Washington, DC: National Aeronautics and Space Administration, 1997.

J, Petersen Brian, Scott David D y United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. A dynamic response model for pressure sensors in continuum and high Knudsen number flows with large temperature gradients. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

1948-, Speziale C. G. y Institute for Computer Applications in Science and Engineering., eds. A modified restricted Euler equation for turbulent flows with mean velocity gradients. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1994.

Hoffenberg, R. Wake measurements in a strong adverse pressure gradient. [Washington, DC: National Aeronautics and Space Administration, 1995.

Hoffenberg, R. Wake measurements in a strong adverse pressure gradient. [Washington, DC: National Aeronautics and Space Administration, 1995.

Baysal, Oktay. Efficient gradient-based shape optimization methodology using inviscid/viscous CFD: Summary of research report for the period of March 9, 1995 to March 8, 1997, grant# NCC-1-211. Norfolk, Va: Dept. of Aerospace Engineering, College of Engineering and Technology, Old Dominion University, 1997.

United States. National Aeronautics and Space Administration., ed. Efficient gradient-based shape optimization methodology using inviscid/viscous CFD: Summary of research report for the period of March 9, 1995 to March 8, 1997, grant# NCC-1-211. Norfolk, Va: Dept. of Aerospace Engineering, College of Engineering and Technology, Old Dominion University, 1997.

United States. National Aeronautics and Space Administration., ed. Efficient gradient-based shape optimization methodology using inviscid/viscous CFD: Summary of research report for the period of March 9, 1995 to March 8, 1997, grant# NCC-1-211. Norfolk, Va: Dept. of Aerospace Engineering, College of Engineering and Technology, Old Dominion University, 1997.

Ingebo, Robert D. Scattered-light scanner measurements of cryogenic liquid-jet breakup. [Washington, D.C: National Aeronautics and Space Administration, 1990.

R, Buchele Donald y United States. National Aeronautics and Space Administration., eds. Scattered-light scanner measurements of cryogenic liquid-jet breakup. [Washington, D.C: National Aeronautics and Space Administration, 1990.

R, Buchele Donald y United States. National Aeronautics and Space Administration., eds. Scattered-light scanner measurements of cryogenic liquid-jet breakup. [Washington, D.C: National Aeronautics and Space Administration, 1990.

Hamed, A. Flow characteristics in boundary layer bleed slots with plenum. [Washington, D.C: National Aeronautics and Space Administration, 1995.

Hamed, A. Flow characteristics in boundary layer bleed slots with plenum. [Washington, D.C: National Aeronautics and Space Administration, 1995.

Brown, James L. The thin oil film equation. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1999.

United States. National Aeronautics and Space Administration. y Massachusetts Institute of Technology. Dept. of Earth, Atmospheric, and Planetary Sciences., eds. Lateral variation in upper mantle temperature and composition beneath mid-ocean ridges inferred from shear-wave propagation, geoid, and bathymetry. [Cambridge, Mass.]: Dept. of Earth, Atmospheric, and Planetary Sciences, Massachusetts Institute of Technology, 1991.

T, Papageorgiou Demetrios, Smyrlis Yiorgos S y Institute for Computer Applications in Science and Engineering., eds. Nonlinear stability of oscillatory core-annular flow: A generalized Kuramoto-Sivashinsky equation with time periodic coefficients. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1994.

A, Sprague Lori. Response of stream chemistry during base flow to gradients of urbanization in selected locations across the conterminous United States, 2002-04. Reston, Va: U.S. Geological Survey, 2007.

B, Gatski T., Speziale C. G. 1948- y Institute for Computer Applications in Science and Engineering., eds. On the prediction of free turbulent jets with swirl using a quadratic pressure-strain model. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, Institute for Computer Applications in Science and Engineering, 1994.

B, Gatski T., Speziale C. G. 1948- y Institute for Computer Applications in Science and Engineering., eds. On the prediction of free turbulent jets with swirl using a quadratic pressure-strain model. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, Institute for Computer Applications in Science and Engineering, 1994.

Choudhari, Meelan. Acoustic receptivity due to weak surface inhomogeneities in adverse pressure gradient boundary layers. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

L, Ng Lian, Streett Craig L y Langley Research Center, eds. Acoustic receptivity due to weak surface inhomogeneities in adverse pressure gradient boundary layers. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

R, Malik Mujeeb y Institute for Computer Applications in Science and Engineering., eds. Effect of crossflow on Görtler instability in incompressible boundary layers. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1994.

United States. National Aeronautics and Space Administration., ed. Numerical solutions of the complete Navier-Stokes equations: Progress report no. 16 for the period July 1, 1998 to December 31, 1989. Raleigh, N.C: Dept. of Mechanical and Aerospace Engineering, North Carolina State University, 1989.

United States. National Aeronautics and Space Administration., ed. Numerical solutions of the complete Navier-Stokes equations: Progress report no. 27 for the period October 1, 1995 to September 30, 1996. Raleigh, N.C: Dept. of Mechanical and Aerospace Engineering, North Carolina State University, 1996.

S, Liou M., Ng Wing y United States. National Aeronautics and Space Administration., eds. Preconditioned conjugate-gradient methods for low-speed flow calculations. [Washington, DC: National Aeronautics and Space Administration, 1993.

S, Liou M., Ng Wing y United States. National Aeronautics and Space Administration., eds. Preconditioned conjugate-gradient methods for low-speed flow calculations. [Washington, DC: National Aeronautics and Space Administration, 1993.

S, Liou M., Ng Wing y United States. National Aeronautics and Space Administration., eds. Preconditioned conjugate-gradient methods for low-speed flow calculations. [Washington, DC: National Aeronautics and Space Administration, 1993.

Meng-Sing, Liou, Ng Wing y United States. National Aeronautics and Space Administration., eds. Preconditioned conjugate-gradient methods for low-speed flow calculations. [Washington, DC: National Aeronautics and Space Administration, 1993.