Books on the topic 'Pressure gradients'

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

McGrath, B. E. Some features of surface pressure fluctuations in turbulent boundary layers with zero and favorable pressure gradients. Langley Research Center, 1987.

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

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

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

M, Kassir S., Larwood S. M, and 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. Aeronautical Engineering Dept., California Polytechnic State University ; [Washington, D.C., 1988.

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

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

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. Clarkson University, 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. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

Center, Langley Research, ed. Effect of pressure gradients on plate response and radiation in a supersonic turbulent boundary layer. National Aeronautics and Space Administration, Langley Research Center, 1997.

K, Notestine Kristopher, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Aerodynamic pressure and heating-rate distributions in tile gaps around chine regions with pressure gradients at a Mach number of 6.6. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

Walker, Nan D. Investigation of pressure and pressure gradients along the Louisiana/Texas inner shelf and their relationships to wind forcing and current variability. U.S. Dept. of the Interior, Minerals Management Service, Gulf of Mexico OCS Region, 2001.

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

A, Kassir J., Larwood S. M, and Ames Research Center, eds. The influence of free-stream turbulence on turbulent boundary layers with mild adverse pressure gradients. National Aeronautics and Space Administration, Ames Research Center, 1989.

A, Kassir J., Larwood S. M, and Ames Research Center, eds. The influence of free-stream turbulence on turbulent boundary layers with mild adverse pressure gradients. National Aeronautics and Space Administration, Ames Research Center, 1989.

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

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

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

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

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

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

Zingg, D. W. Higher-order approximations in interactive airfoil calculations. 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. National Aeronautics and Space Administration, 1987.

Zingg, D. W. Higher-order approximations in interactive airfoil calculations. Institute for Aerospace Studies, 1988.

J, Petersen Brian, Scott David D, and 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. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., ed. Modification of a variational objective analysis model for new equations for pressure gradient and vertical velocity in the lower troposphere and for spatial resolution and accuracy of satellite data. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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

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

Elrod, David Alan. A comparison of experimental and theoretical results for leakage, pressure gradients, and rotordynamic coefficients for tapered annular gas seal: Progress report. National Aeronautics and Space Administration, 1986.

T, Papageorgiou Demetrios, Smyrlis Yiorgos S, and 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. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1994.

Hamed, A. Flow characteristics in boundary layer bleed slots with plenum. National Aeronautics and Space Administration, 1995.

Hamed, A. Flow characteristics in boundary layer bleed slots with plenum. National Aeronautics and Space Administration, 1995.

M, Kassir S., Larwood S. M, and 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. Aeronautical Engineering Dept., California Polytechnic State University ; [Washington, D.C., 1988.

M, Kassir S., Larwood S. M, and 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. Aeronautical Engineering Dept., California Polytechnic State University ; [Washington, D.C., 1988.

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

Wang, Ningli, ed. Intraocular and Intracranial Pressure Gradient in Glaucoma. Springer Singapore, 2019. http://dx.doi.org/10.1007/978-981-13-2137-5.

Environmental Technology Laboratory (Environmental Research Laboratories), ed. Pressure-gradient, velocity-velocity structure function for locally isotropic turbulence in incompressible fluid. U.S. Dept. of Commerce, National Oceanic and Atmospheric Administration, Environmental Research Laboratories, Environmental Technology Laboratory, 1997.

Environmental Technology Laboratory (Environmental Research Laboratories), ed. Pressure-gradient, velocity-velocity structure function for locally isotropic turbulence in incompressible fluid. U.S. Dept. of Commerce, National Oceanic and Atmospheric Administration, Environmental Research Laboratories, Environmental Technology Laboratory, 1997.

Hill, Reginald J. Pressure-gradient, velocity-velocity structure function for locally isotropic turbulence in incompressible fluid. U.S. Dept. of Commerce, National Oceanic and Atmospheric Administration, Environmental Research Laboratories, Environmental Technology Laboratory, 1997.

Hill, Reginald J. Pressure-gradient, velocity-velocity structure function for locally isotropic turbulence in incompressible fluid. U.S. Dept. of Commerce, National Oceanic and Atmospheric Administration, Environmental Research Laboratories, Environmental Technology Laboratory, 1997.