Books on the topic 'Boundary layer flow'
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United States. National Aeronautics and Space Administration., ed. Supersonic boundary-layer flow turbulence modeling. National Aeronautics and Space Administration, 1993.
Find full textUnited States. National Aeronautics and Space Administration., ed. Supersonic boundary-layer flow turbulence modeling. National Aeronautics and Space Administration, 1993.
Find full textUnited States. National Aeronautics and Space Administration., ed. Supersonic boundary-layer flow turbulence modeling. National Aeronautics and Space Administration, 1993.
Find full textJoslin, Ronald D. Active control of instabilities in laminar boundary-layer flow. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1994.
Find full textHerbert, Th. Boundary-layer transition - analysis and prediction revisted. American Institute of Aeronautics and Astronautics, 1991.
Find full textInstitute for Computer Applications in Science and Engineering., ed. Modelling the transitional boundary layer. National Aeronautics and Space Administration, Langley Research Center, Institute for Computer Applications in Science and Engineering, 1990.
Find full textJ, Clifford N., French J. R, and Hardisty J. 1955-, eds. Turbulence: Perspectives on flow and sediment transport. Wiley, 1993.
Find full textLysenko, V. I. Stability characteristics of a supersonic boundary layer and their relation to the position of the laminar-turbulent transition point. National Aeronautics and Space Administration, 1987.
Find full textUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Distributed acoustic receptivity in laminar flow control configurations. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.
Find full text1933-, Nayfeh Ali Hasan, and Langley Research Center, eds. Stability of separating subsonic boundary layers. National Aeronautics and Space Administration, Langley Research Center, 1994.
Find full text1933-, Nayfeh Ali Hasan, and Langley Research Center, eds. Stability of separating subsonic boundary layers. National Aeronautics and Space Administration, Langley Research Center, 1994.
Find full textGoldstein, Marvin E. The effect of nonlinear critical layers on boundary layer transition. National Aeronautics and Space Administration, 1995.
Find full textSchofield, W. H. Viscous flow around wall mounted obstacles. Aeronautical Research Laboratories, 1986.
Find full textNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Computation of Three-Dimensional Boundary Layers Including Separation. s.n, 1987.
Find full textNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Computation of three-dimensional boundary layers including separation. AGARD, 1987.
Find full textE, Smith G., and United States. National Aeronautics and Space Administration., eds. On supersonic-inlet boundary-layer bleed flow. National Aeronautics and Space Administration, 1995.
Find full textHarloff, G. J. On supersonic-inlet boundary-layer bleed flow. National Aeronautics and Space Administration, 1995.
Find full textHarloff, G. J. On supersonic-inlet boundary-layer bleed flow. National Aeronautics and Space Administration, 1995.
Find full textHaw, Richard C. The effects of forcing on a single stream shear layer and its parent boundary layer. College of Engineering, Michigan State University, 1990.
Find full textNelson, P. A. An algorithm for the automatic control of boundary layer flow. University of Southampton, Institute of Sound and Vibration Research, 1994.
Find full textAnalytical Services & Materials, Inc. and Langley Research Center, eds. Effect of suction on controlling the secondary instability of boundary layers. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
Find full textJ, Holmes Bruce, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Flight-measured laminar boundary-layer transition phenomena including stability theory analysis. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
Find full textCenter, Langley Research, ed. Stability of the flow around a cylinder: The spin-up problem. National Aeronautics and Space Administration, Langley Research Center, 1991.
Find full textKhalid, M. Turbulent boundary layer solution for two-dimensional compressible flow using mixing length and K-e turbulence models. National Research Council Canada, Institute for Aerospace Research, 1990.
Find full textUnited States. National Aeronautics and Space Administration., ed. Parametric study on laminar flow for finite wings at supersonic speeds. National Aeronautics and Space Administration, 1994.
Find full textJoslin, Ronald D. Overview of laminar flow control. National Aeronautics and Space Administration, Langley Research Center, 1998.
Find full text1940-, Rahman M., ed. Laminar and turbulent boundary layers. Computational Mechanics Publication, 1997.
Find full textSibanda, Precious. Boundary layer stability and cross-flow vortices in compressible flows. University of Manchester, 1996.
Find full textArebi, Mohamad Mokhtar Ali. Hydrodynamic stability and cross-flow vortices in boundary layer flows. Universityof Manchester, 1996.
Find full textCenter, Ames Research, ed. Investigation of low-speed turbulent separated flow around airfoils. National Aeronautics and Space Administration, Ames Research Center, 1988.
Find full textCenter, Ames Research, ed. Investigation of low-speed turbulent separated flow around airfoils. National Aeronautics and Space Administration, Ames Research Center, 1988.
Find full textUnited States. National Aeronautics and Space Administration., ed. A three-dimensional turbulent separated flow and related measurements. College of Engineering, Virginia Polytechnic Institute and State University, 1985.
Find full textUnited States. National Aeronautics and Space Administration., ed. A three-dimensional turbulent separated flow and related measurements. College of Engineering, Virginia Polytechnic Institute and State University, 1985.
Find full textPhilip, Hall, and Langley Research Center, eds. Concerning the interaction of non-stationary cross-flow vortices in a three-dimensional boundary layer. National Aeronautics and Space Administration, Langley Research Center, 1990.
Find full textMaestrello, Lucio. Active transition fixing and control of the boundary layer in air. AIAA, 1985.
Find full textMueller, Thomas J. The structure of separated flow regions occurring near the leading edge of airfoils - including transition. Dept. of Aerospace and Mechanical Engineering, University of Notre Dame, 1985.
Find full textUnited States. National Aeronautics and Space Administration., ed. Three dimensional boundary layers in internal flows. National Aeronautics and Space Administration, 1987.
Find full textCenter, Langley Research, ed. Instability of flow in a streamwise corner. National Aeronautics and Space Administration, Langley Research Center, 1992.
Find full textStephen, Cowley, Hall Philip, and Langley Research Center, eds. On the instability of hypersonic flow past a flat plate. National Aeronautics and Space Administration, Langley Research Center, 1990.
Find full textKogan, M. N. Receptivity of flat-plate boundary layer in a non-uniform free stream (vorticity normal to the plate): Under cooperative agreement NCC1-241. National Aeronautics and Space Administration, Langley Research Center, 1997.
Find full textV, Ustinov M., and Langley Research Center, eds. Receptivity of flat-plate boundary layer in a non-uniform free stream (vorticity normal to the plate): Under cooperative agreement NCC1-241. National Aeronautics and Space Administration, Langley Research Center, 1997.
Find full textKogan, M. N. Receptivity of flat-plate boundary layer in a non-uniform free stream (vorticity normal to the plate): Under cooperative agreement NCC1-241. National Aeronautics and Space Administration, Langley Research Center, 1997.
Find full textKogan, M. N. Receptivity of flat-plate boundary layer in a non-uniform free stream (vorticity normal to the plate): Under cooperative agreement NCC1-241. National Aeronautics and Space Administration, Langley Research Center, 1997.
Find full textKogan, M. N. Receptivity of flat-plate boundary layer in a non-uniform free stream (vorticity normal to the plate). National Aeronautics and Space Administration, Langley Research Center, 1997.
Find full textCenter, Ames Research, ed. Flow unsteadiness effects on boundary layers. NASA Ames Research Center, 1989.
Find full textK, Hebbar Sheshagiri, and Ames Research Center, eds. Three-dimensional turbulent boundary layer flow over a spinning cylinder. National Aeronautics and Space Administration, Ames Research Center, 1991.
Find full textDriver, David M. Three-dimensional turbulent boundary layer flow over a spinning cylinder. National Aeronautics and Space Administration, Ames Research Center, 1991.
Find full textDriver, David M. Three-dimensional turbulent boundary layer flow over a spinning cylinder. National Aeronautics and Space Administration, Ames Research Center, 1991.
Find full textDriver, David M. Three-dimensional turbulent boundary layer flow over a spinning cylinder. National Aeronautics and Space Administration, Ames Research Center, 1991.
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