Книги з теми "Edge layer"
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J, Shamroth S., Langley Research Center, and Scientific Research Associates, eds. On the application of a hairpin vortex model of wall turbulence to trailing edge noise prediction. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.
Знайти повний текст джерелаLin, N. Receptivity of the boundary layer on a semi-infinite flat plate with an elliptic leading edge. Tempe, Ariz: Arizona State University, Department of Mechanical and Aerospace Engineering, 1989.
Знайти повний текст джерелаMueller, Thomas J. The structure of separated flow regions occurring near the leading edge of airfoils - including transition. Notre Dame, Ind: Dept. of Aerospace and Mechanical Engineering, University of Notre Dame, 1985.
Знайти повний текст джерелаHulshoff, Steven John. The response of the unsteady laminar boundary layer to leading edge acoustic diffraction. [Downsview, Ont.]: Department of Aerospace Science and Engineering, 1989.
Знайти повний текст джерелаInstitute for Computer Applications in Science and Engineering., ed. Görtler vortices in growing boundary layers: The leading edge receptivity problem, linear growth and the nonlinear breakdown stage. Hampton, Va: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1989.
Знайти повний текст джерелаInstitute for Computer Applications in Science and Engineering., ed. Görtler vortices in growing boundary layers: The leading edge receptivity problem, linear growth and the nonlinear breakdown stage. Hampton, Va: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1989.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Analysis of the leading edge effects on the boundary layer transition: Technical report, March 1, 1984 - August 31, 1990. [Washington, DC: National Aeronautics and Space Administration, 1990.
Знайти повний текст джерелаCenter, Ames Research, and United States. National Aeronautics and Space Administration., eds. Boundary layer transition in the leading edge region of a swept cylinder in high speed flow. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1998.
Знайти повний текст джерелаJ, Ghosn Louis, Miller Robert A. 1947-, and Lewis Research Center, eds. Effect of layer-graded bond coats on edge stress concentration and oxidation behavior of thermal barrier coatings. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.
Знайти повний текст джерелаJ, Ghosn Louis, Miller Robert A. 1947-, and Lewis Research Center, eds. Effect of layer-graded bond coats on edge stress concentration and oxidation behavior of thermal barrier coatings. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.
Знайти повний текст джерелаJ, Ghosn Louis, Miller Robert A. 1947-, and Lewis Research Center, eds. Effect of layer-graded bond coats on edge stress concentration and oxidation behavior of thermal barrier coatings. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.
Знайти повний текст джерелаMueller, T. J. The structure of separated flow regions occurring near the leading edge of airfoils, including transition: Semi-annual status report, February 1986-July 1986. [Washington, D.C: National Aeronautics and Space Administration, 1986.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. The structure of separated flow regions occurring near the leading edge of airfoils, including transition: Semi-annual status report, November 1984 - April 1985. Notre Dame, Ind: Dept. of Aerospace and Mechanical Engineering, University of Notre Dame, 1985.
Знайти повний текст джерелаNicolas, Spitz, and NASA Glenn Research Center, eds. Predicting modes of the unsteady vorticity field near the trailing edge of a blade. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2003.
Знайти повний текст джерелаNicolas, Spitz, and NASA Glenn Research Center, eds. Predicting modes of the unsteady vorticity field near the trailing edge of a blade. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2003.
Знайти повний текст джерелаA, Campbell Bryan, and Langley Research Center, eds. Subsonic investigation of a leading-edge boundary layer cont[r]ol suction system on a high-speed civil transport configuration. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.
Знайти повний текст джерелаA, Campbell Bryan, and Langley Research Center, eds. Subsonic investigation of a leading-edge boundary layer cont[r]ol suction system on a high-speed civil transport configuration. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.
Знайти повний текст джерелаLessard, Victor R. Low speed analysis of mission adaptive flaps on a high speed civil transport configuration. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.
Знайти повний текст джерелаLessard, Victor R. Low speed analysis of mission adaptive flaps on a high speed civil transport configuration. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.
Знайти повний текст джерелаCenter, Langley Research, ed. Supersonic leading edge receptivity. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.
Знайти повний текст джерелаKogan, M. N. Receptivity of flat-plate boundary layer in a non-uniform free stream (vorticity normal to the plate): Under cooperative agreement NCC1-241. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.
Знайти повний текст джерелаKogan, M. N. Receptivity of flat-plate boundary layer in a non-uniform free stream (vorticity normal to the plate): Under cooperative agreement NCC1-241. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.
Знайти повний текст джерелаKogan, M. N. Receptivity of flat-plate boundary layer in a non-uniform free stream (vorticity normal to the plate). Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.
Знайти повний текст джерелаKogan, M. N. Receptivity of flat-plate boundary layer in a non-uniform free stream (vorticity normal to the plate): Under cooperative agreement NCC1-241. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.
Знайти повний текст джерелаV, 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. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.
Знайти повний текст джерелаCenter, Ames Research, ed. Rotor vortex filaments: Living on the slipstream's edge. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1997.
Знайти повний текст джерелаAmerican Bar Association. Section of State and Local Government Law, ed. At the cutting edge 2009: Land use law from The urban lawyer. Chicago, Ill: American Bar Association, Section of State and Local Government Law, 2010.
Знайти повний текст джерелаMerriam, Dwight H. At the cutting edge 2009: Land use law from The urban lawyer. Edited by American Bar Association. Section of State and Local Government Law. Chicago, Ill: American Bar Association, Section of State and Local Government Law, 2010.
Знайти повний текст джерелаAmerican Bar Association. Section of State and Local Government Law, ed. At the cutting edge, 2010: Land use law from The Urban Lawyer. Chicago, Ill: American Bar Association, Section of State and Local Government Law, 2011.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Numerical studies of boundary-layer receptivity: A progress report. [Washington, DC: National Aeronautics and Space Administration, 1995.
Знайти повний текст джерелаSampson, C. Garth. Nightfire Island: Later Holocene lakemarsh adaptation on the western edge of the Great Basin. Eugene, Or: Dept. of Anthropology, University of Oregon, 1985.
Знайти повний текст джерелаSampson, C. Garth. Nightfire Island: Later Holocene lakemarsh adaptation on the western edge of the Great Basin. Eugene, Or: Dept. of Anthropology, University of Oregon, 1985.
Знайти повний текст джерелаMelvin, Aikens C., ed. Nightfire Island: Later Holocene lakemarsh adaptation on the western edge of the Great Basin. Eugene, Or: Dept. of Anthropology, University of Oregon, 1985.
Знайти повний текст джерелаWitzigmann, Bernd. Design and implementation of a three-dimensional edge emitting quantum well laser simulator / Bernd Witzigmann. Konstanz: Hartung-Gorre, 2000.
Знайти повний текст джерелаR, Sarma Garimella, Mangalam Siva M, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Flight demonstration of a shock location sensor using constant voltage hot-film anemometry. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.
Знайти повний текст джерелаMario, Vargas, and United States. National Aeronautics and Space Administration., eds. A laser-based ice shape profilometer for use in icing wind tunnels. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.
Знайти повний текст джерелаMario, Vargas Meza, and United States. National Aeronautics and Space Administration., eds. A laser-based ice shape profilometer for use in icing wind tunnels. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.
Знайти повний текст джерелаMario, Vargas, and United States. National Aeronautics and Space Administration., eds. A laser-based ice shape profilometer for use in icing wind tunnels. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.
Знайти повний текст джерелаMario, Vargas, and United States. National Aeronautics and Space Administration., eds. A laser-based ice shape profilometer for use in icing wind tunnels. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.
Знайти повний текст джерелаHall, Philip. Gortler vortices in growing boundary layers: the leading edge receptivity problem, linear growth and the nonlinear breakdown stage. Hampton, Va: Institute for Computer Applications in Science and Engineering, 1989.
Знайти повний текст джерелаD, Saunders J., and United States. National Aeronautics and Space Administration., eds. 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet. [Washington, DC]: National Aeronautics and Space Administration, 1995.
Знайти повний текст джерелаD, Saunders J., and United States. National Aeronautics and Space Administration., eds. 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet. [Washington, DC]: National Aeronautics and Space Administration, 1995.
Знайти повний текст джерелаD, Saunders J., and United States. National Aeronautics and Space Administration., eds. 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet. [Washington, DC]: National Aeronautics and Space Administration, 1995.
Знайти повний текст джерелаD, Saunders J., and United States. National Aeronautics and Space Administration., eds. 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet. [Washington, DC]: National Aeronautics and Space Administration, 1995.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Control of unsteady separated flow associated with the dynamic stall of airfoils: Final report, 95-09. San Jose, CA: MCAT Institute, 1995.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Control of unsteady separated flow associated with the dynamic stall of airfoils. San Jose, CA: MCAT Institute, 1994.
Знайти повний текст джерелаE, Mineck Raymond, and Langley Research Center, eds. Assessment of dual-point drag reduction for an executive-jet modified airfoil section. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.
Знайти повний текст джерелаAllison, Dennis O. Assessment of dual-point drag reduction for an executive-jet modified airfoil section. Hampton, Virginia: National Aeronautics and Space Administration, Langly Research Center, 1996.
Знайти повний текст джерелаE, Mineck Raymond, and Langley Research Center, eds. Assessment of dual-point drag reduction for an executive-jet modified airfoil section. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Finite-element analysis of a Mach-8 flight test article using nonlinear contact elements. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.
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