Books on the topic 'Boundary-Layer Separation'

Smith, Frank T., and Susan N. Brown, eds. Boundary-Layer Separation. Berlin, Heidelberg: Springer Berlin Heidelberg, 1987. http://dx.doi.org/10.1007/978-3-642-83000-6.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Computation of Three-Dimensional Boundary Layers Including Separation. S.l: s.n, 1987.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Computation of three-dimensional boundary layers including separation. Neuilly sur Seine, France: AGARD, 1987.

Chang, Paul K. Recent development in flow separation. Seoul, Korea: Pang Han Pub. Co., 1985.

United States. National Aeronautics and Space Administration., ed. Turbulent boundary layer separation over a rearward facing ramp and its control through mechanical excitation. [Washington, DC]: National Aeronautics and Space Administration, 1991.

Duck, Peter W. Three-dimensional marginal separation. Hampton, Va: Institute for Computational Mechanics in Propulsion, 1988.

United States. National Aeronautics and Space Administration., ed. Three-dimensional marginal separation. [Washington, D.C.]: National Aeronautics and Space Administration, 1989.

United States. National Aeronautics and Space Administration., ed. Three-dimensional marginal separation. [Washington, D.C.]: National Aeronautics and Space Administration, 1989.

United States. National Aeronautics and Space Administration., ed. Three-dimensional marginal separation. [Washington, D.C.]: National Aeronautics and Space Administration, 1989.

Dommelen, Leon L. van. On the Lagrangian description of unsteady boundary layer separation. [Washington, D.C.]: National Aeronautics and Space Administration, 1989.

Selby, Gregory V. Jet vortex generators for turbulent flow separation control. Norfolk, Va: Old Dominion University Research Foundation, 1990.

G, Bakker P., Henkes, R. A. W. M., and Ingen J. L. van, eds. Boundary-layer separation in aicraft aerodynamics: Proceedings of the seminar held on 6 February 1997 in Delft, dedicated to professor J.L. van Ingen. Delft: Delft University Press, 1997.

Lewis Research Center. Institute for Computational Mechanics in Propulsion., ed. Unsteady three-dimensional marginal separation, including breakdown. [Washington, D.C.]: NASA, 1990.

Lewis Research Center. Institute for Computational Mechanics in Propulsion., ed. Unsteady three-dimensional marginal separation, including breakdown. [Washington, D.C.]: NASA, 1990.

Duck, Peter W. Unsteady three-dimensional marginal separation, including breakdown. [Washington, D.C.]: NASA, 1990.

1933-, Nayfeh Ali Hasan, and Langley Research Center, eds. Stability of separating subsonic boundary layers. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

1933-, Nayfeh Ali Hasan, and Langley Research Center, eds. Stability of separating subsonic boundary layers. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

Smith, Frank T. Boundary-Layer Separation: Proceedings of the IUTAM Symposium London, August 26-28, 1986. Berlin, Heidelberg: Springer Berlin Heidelberg, 1987.

Patrick, William P. Flowfield measurements in a separated and reattached flat plate turbulent boundary layer. Cleveland, Ohio: Lewis Research Center, 1987.

Dommelen, Leon Van. On the Lagrangian description of unsteady boundary layer separation.: I - General theory. Cleveland, Ohio: Institute for Computational Mechanics in Propulsion, 1989.

Dommelen, Leon L. Van. On the Lagrangian description of unsteady boundary layer separation.: II - The spinning sphere. Cleveland, Ohio: Institute for Computational Mechanics in Propulsion, 1989.

Schofield, W. H. Viscous flow around wall mounted obstacles. Melbourne, Australia: Aeronautical Research Laboratories, 1986.

Hamed, A. Flow separation in shock wave boundary layer interactions at hypersonic speeds. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

Philip, Hall, and Langley Research Center, eds. Fully nonlinear Görtler vortices in constricted channel flows and their effect on the onset of separation. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

Philip, Hall, and Langley Research Center, eds. Fully nonlinear Görtler vortices in constricted channel flows and their effect on the onset of separation. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

Philip, Hall, and Langley Research Center, eds. Fully nonlinear Görtler vortices in constricted channel flows and their effect on the onset of separation. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

Doerffer, Piotr. Unsteady effects of shock wave induced separation. Berlin: Springer, 2010.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Calculation of 3D separated turbulent flows in boundary layer limit. Neuilly sur Seine, France: AGARD, 1990.

1948-, Smith F. T., Brown S. N. 1937-, International Union of Theoretical and Applied Mechanics., and IUTAM Symposium on Boundary-Layer Separation (1986 : London, England), eds. Boundary-layer separation: Proceedings of the IUTAM Symposium, London, August 26-28, 1986. Berlin: Springer-Verlag, 1987.

R, Hingst Warren, and United States. National Aeronautics and Space Administration., eds. Use of surface heat transfer measurements as a flow separation diagnostic in a two-dimensional reflected oblique shock/turbulent boundary layer interaction. [Washington, DC: National Aeronautics and Space Administration, 1993.

1944-, Carter James E., Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Analysis of transitional separation bubbles on infinite swept wings. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

W, Barter J., and United States. National Aeronautics and Space Administration., eds. Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction: Final report on NASA grant NAG 1-1471 for the period 01/09/93 through 01/01/95. Austin, Tex: Center for Aerodynamics Research, Dept. of Aerospace Engineering & Engineering Mechanics, University of Texas at Austin, 1995.

W, Barter J., and United States. National Aeronautics and Space Administration., eds. Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction: Final report on NASA grant NAG 1-1471 for the period 01/09/93 through 01/01/95. Austin, Tex: Center for Aerodynamics Research, Dept. of Aerospace Engineering & Engineering Mechanics, University of Texas at Austin, 1995.

W, Barter J., and United States. National Aeronautics and Space Administration., eds. Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction: Final report on NASA grant NAG 1-1471 for the period 01/09/93 through 01/01/95. Austin, Tex: Center for Aerodynamics Research, Dept. of Aerospace Engineering & Engineering Mechanics, University of Texas at Austin, 1995.

L, Van Dommelen Leon, Lam Shui T, and Langley Research Center, eds. On the use of Lagrangian variables in descriptions of unsteady boundary-layer separation. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

E, Ashpis D., and NASA Glenn Research Center, eds. Demonstration of separation delay with glow-discharge plasma actuators. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2003.

E, Ashpis D., and NASA Glenn Research Center, eds. Demonstration of separation delay with glow-discharge plasma actuators. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2003.

Saeed, Farokhi, and United States. National Aeronautics and Space Administration., eds. A study of three dimensional turbulent boundary layer separation and vortex flow control using the reduced Navier Stokes equations. [Washington, DC]: National Aeronautics and Space Administration, 1991.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Special course on three-dimensional supersonic/hypersonic flows including separation. Neuilly-sur-Seine: AGARD, 1990.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Special course on three-dimensional supersonic/hypersonic flows including separation. Neuilly sur Seine, France: AGARD, 1990.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Calculation of 3D separated turbulent flows in boundary layer limit: Report of the fluid dynamics panel working group 10. Neuilly-sur-Seine: AGARD, 1990.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Vortex flow aerodynamics. Neuilly-sur-Seine: AGARD, 1991.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Vortex flow aerodynamics. Neuilly sur Seine, France: AGARD, 1991.

Old Dominion University. Research Foundation. and Langley Research Center, eds. Experimental parametric study of jet vortex generators for flow separation control. Norfolk, Va: Old Dominion University Research Foundation, 1991.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., ed. Flow-separation patterns on symmetric forebodies. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., ed. Flow-separation patterns on symmetric forebodies. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

Keener, Earl R. Flow-separation patterns on symmetric forebodies. Moffett Field, Calif: Ames Research Center, 1986.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., ed. Flow-separation patterns on symmetric forebodies. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

R, Bristow Dean, McDonnell Aircraft Company, and Langley Research Center, eds. Numerical approach for the aerodynamic analysis of airfoils with laminar separation. St. Louis, Mo: McDonnel Douglas Corporation, McDonnel Aircraft Company, 1985.

L, Roach Robert, and United States. National Aeronautics and Space Administration., eds. A Fast, uncoupled, compressible, two-dimensional, unsteady boundary layer algorithm with separation for engine inlets. [Washington, DC]: National Aeronautics and Space Administration, 1992.