Книги з теми "Boundary-Layer Instability"
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Seddougui, Sharon O. Surface-cooling effects on compressible boundary-layer instability. Hampton, Va: Institute for Computer Applications in Science and Engineering, 1990.
Знайти повний текст джерелаEl-Hady, Nabil M. Spatial three-dimensional secondary instability of compressible boundary-layer flows. Hampton, Va: Langley Research Center, 1989.
Знайти повний текст джерелаHall, Philip. On the instability of boundary layers on heated flat plates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.
Знайти повний текст джерелаIUTAM Symposium (1993 Potsdam, N.Y.). Nonlinear instability of nonparallel flows. Berlin: Springer-Verlag, 1994.
Знайти повний текст джерелаHall, Philip. On the modulational instability of large amplitude waves in supersonic boundary layers. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1995.
Знайти повний текст джерелаHall, Philip. The inviscid secondary instability of fully nonlinear longitudinal vortex structures in growing boundary layers. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.
Знайти повний текст джерелаSmith, A. Instability and transition of flow at, and near, an attachment-line: Including control by surface suction. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.
Знайти повний текст джерелаHall, Philip. An asymptotic investigation of the stationary modes of instability of the boundary layer on a rotating disc. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.
Знайти повний текст джерелаCanright, David. Rayleigh-Taylor instability of a viscous film overlying a pasive fluid. Monterey, Calif: Naval Postgraduate School, 1989.
Знайти повний текст джерелаSeddougui, Sharon O. A nonlinear investigation of the stationary mode of instability of the three-dimensional compressible boundary layer due to a rotating disc. Hampton, Va: ICASE, 1989.
Знайти повний текст джерелаUwe, Dallmann, and Deutsche Forschungs- und Versuchsanstalt für Luft- und Raumfahrt., eds. Theoretical investigation of secondary instability of three-dimensional boundary-layer flows with application to the DFVLR-F5 model wing. Koln: DFVLR, 1987.
Знайти повний текст джерелаMaestrello, Lucio. Numerical study of three-dimensional spatial instability of a supersonic flat plate boundary layer. Hampton, Va: ICASE, 1989.
Знайти повний текст джерелаLin, S. P. Nonlinear Instability of Nonparallel Flows: IUTAM Symposium Potsdam, NY, USA July 26-31, 1993. Berlin, Heidelberg: Springer Berlin Heidelberg, 1994.
Знайти повний текст джерелаOtto, S. R. The effect of crossflow on Görtler vortices. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1994.
Знайти повний текст джерелаIUTAM Symposium on Nonlinear Instability and Transition in Three-Dimensional Boundary Layers (1995 Manchester, England). IUTAM Symposium on Nonlinear Instability and Transition in Three-Dimensional Boundary Layers: Proceedings of the IUTAM Symposium held in Manchester, UK, 17-20 July 1995. Dordrecht: Kluwer Academic, 1996.
Знайти повний текст джерелаFu, Yibin B. Effects of Gortler vortices, wall cooling and gas dissociation on the Rayleigh instability in a hypersonic boundary layer. Hampton, Va: Institute for Computer Applications in Science and Engineering, 1991.
Знайти повний текст джерелаDuck, Peter W. IUTAM Symposium on Nonlinear Instability and Transition in Three-Dimensional Boundary Layers: Proceedings of the IUTAM Symposium held in Manchester, U.K., 17-20 July 1995. Dordrecht: Springer Netherlands, 1996.
Знайти повний текст джерелаWendt, Volker. Experimentelle Untersuchung der Instabilitat von ebenen und konischen laminaren Hyperschallgrenzschichten. Koln, Germany: DLR, 1993.
Знайти повний текст джерелаI, Bowles R., Smith F. T. 1948-, and Langley Research Center, eds. Surface--cooling effects on compressible boundary--layer instability. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.
Знайти повний текст джерелаI, Bowles R., Smith F. T. 1948-, and Langley Research Center, eds. Surface--cooling effects on compressible boundary--layer instability. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. Spatial three-dimensional secondary instability of compressible boundary-layer flows. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. Spatial three-dimensional secondary instability of compressible boundary-layer flows. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. Secondary instability of compressible boundary layer to subharmonic three-dimensional disturbances. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Relationship between transition and modes of instability in supersonic boundary layers. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Program, 1993.
Знайти повний текст джерелаNational Aeronautics and Space Administration (NASA) Staff. Surface-Cooling Effects on Compressible Boundary-Layer Instability. Independently Published, 2018.
Знайти повний текст джерелаTheofilis, Vassilis, and Julio Soria. Instability and Control of Massively Separated Flows. Springer, 2016.
Знайти повний текст джерелаCenter, Langley Research, ed. Instability of flow in a streamwise corner. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.
Знайти повний текст джерелаTheofilis, Vassilis, and Julio Soria. Instability and Control of Massively Separated Flows: Proceedings of the International Conference on Instability and Control of Massively Separated Flows, Held in Prato, Italy, from 4-6 September 2013. Springer, 2015.
Знайти повний текст джерелаTheofilis, Vassilis, and Julio Soria. Instability and Control of Massively Separated Flows: Proceedings of the International Conference on Instability and Control of Massively Separated Flows, Held in Prato, Italy, from 4-6 September 2013. Springer, 2015.
Знайти повний текст джерелаAnalytical Services & Materials, Inc. and Langley Research Center, eds. Effect of suction on controlling the secondary instability of boundary layers. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
Знайти повний текст джерелаStephen, Cowley, Hall Philip, and Langley Research Center, eds. On the instability of hypersonic flow past a flat plate. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.
Знайти повний текст джерелаR, Malik Mujeeb, and 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.
Знайти повний текст джерелаCenter, Langley Research, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Nonparallel instability of supersonic and hypersonic boundary layers. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.
Знайти повний текст джерелаA, Poll D. I., and United States. National Aeronautics and Space Administration., eds. Instability and transition of flow at, and near, an attachment-line: Including control by surface suction : contract number NCC1-218. [Washington, DC: National Aeronautics and Space Administration, 1996.
Знайти повний текст джерелаA phase equation approach to boundary layer instability theory: Tollmien Schlichting waves. Hampton, Va: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1994.
Знайти повний текст джерелаNonlinear interaction of detuned instability waves in boundary-layer transition: Amplitude equations. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.
Знайти повний текст джерелаCenter, Lewis Research, ed. Nonlinear interaction of detuned instability waves in boundary-layer transition: Resonant-triad interaction. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.
Знайти повний текст джерелаAlvin, Bayliss, Krishnan Ramachander, and Langley Research Center, eds. Numerical study of three-dimensional spatial instability of a supersonic flat plate boundary layer. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.
Знайти повний текст джерелаNumerical study of three-dimensional spatial instability of a supersonic flat plate boundary layer. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.
Знайти повний текст джерелаVortex instabilities in 3D boundary layers: The relationship between Görtler and crossflow vortices. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1990.
Знайти повний текст джерелаLin, S. P., and William R. Phillips. Nonlinear Instability of Nonparallel Flows: Iutam Symposium Potsdam, Ny, 1993 (I U T a M - Symposien). Springer, 1994.
Знайти повний текст джерела(Editor), Peter W. Duck, and Philip Hall (Editor), eds. IUTAM Symposium on Nonlinear Instability and Transition in Three-Dimensional Boundary Layers (Fluid Mechanics and Its Applications). Springer, 1996.
Знайти повний текст джерелаSimulation of crossflow instability on a supersonic highly swept wing. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.
Знайти повний текст джерелаWeakly nonparallel and curvature effects on stationary crossflow instability: Comparison of results from multiple-scales analysis and parabolized stability equations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.
Знайти повний текст джерелаAnalytical Services & Materials, Inc. and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Secondary instability of high-speed flows and the influence of wall cooling and suction. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.
Знайти повний текст джерелаPhilip, Hall, and Langley Research Center, eds. Effects of Görtler vortices, wall cooling and gas dissociation on the Rayleigh instability in a hypersonic boundary layer. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.
Знайти повний текст джерелаPhilip, Hall, and Langley Research Center, eds. Effects of Görtler vortices, wall cooling and gas dissociation on the Rayleigh instability in a hypersonic boundary layer. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.
Знайти повний текст джерелаHall, Philip, and Peter W. Duck. IUTAM Symposium on Nonlinear Instability and Transition in Three-Dimensional Boundary Layers: Proceedings of the IUTAM Symposium held in Manchester, U.K., 17-20 July 1995. Springer, 2011.
Знайти повний текст джерелаOn the Görtler instability in hypersonic flows: Sutherland law fluids and real gas effects. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, Institute for Computer Applications in Science and Engineering, 1990.
Знайти повний текст джерелаOn the Görtler instability in hypersonic flows: Sutherland law fluids and real gas effects. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, Institute for Computer Applications in Science and Engineering, 1990.
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