Książki na temat „Shockwave Boundary Layer Interactions”

R, Hingst W., i United States. National Aeronautics and Space Administration., red. Surface and flow field measurements in a symmetric crossing shockwave/turbulent boundary-layer interaction. [Washington, DC]: National Aeronautics and Space Administration, 1993.

Délery, J. Shock-wave boundary layer interactions. Neuilly sur Seine, France: NATO, Advisory Group for Aerospace Research and Development, 1986.

Babinsky, Holger, i John K. Harvey, red. Shock Wave–Boundary-Layer Interactions. Cambridge: Cambridge University Press, 2011. http://dx.doi.org/10.1017/cbo9780511842757.

Shock wave-boundary layer interactions. Cambridge: Cambridge University Press, 2011.

Delery, J. Shock-wave boundary layer interactions. Neuilly sur Seine: Agard, 1986.

IUTAM Symposium (1985 Palaiseau, France). Turbulent shear-layer/shock-wave interactions. Redaktorzy Délery J. 1939-, International Union of Theoretical and Applied Mechanics. i France. Office national d'études et de recherches aérospatiales. Berlin: Springer-Verlag, 1986.

Arellano, Jordi Vilà-Guerau de. Atmospheric boundary layer: Integrating air chemistry and land interactions. New York, NY: Cambridge University Press, 2015.

Blackaby, Nicholas D. Tollmien-Schlichting/vortex interactions in compressible boundary layer flows. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

Blackaby, Nicholas D. Tollmien-Schlichting/vortex interactions in compressible boundary layer flows. Hampton, Va: Institute for Computer Applications in Science and Engineering, 1993.

United States. National Aeronautics and Space Administration., red. Experimental studies of hypersonic shock-wave boundary-layer interactions. Arlington, Tex: University of Texas at Arlington, 1992.

Blackaby, Nicholas D. Tollmien-Schlichting/vortex interactions in compressible boundary layer flows. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

Blackaby, Nicholas D. Tollmien-Schlichting/vortex interactions in compressible boundary layer flows. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

United States. National Aeronautics and Space Administration., red. Turbulence modeling in shock wave/turbulent boundary layer interactions: Final report. [Washington, DC: National Aeronautics and Space Administration, 1992.

Stratosphere troposphere interactions: An introduction. [New York?]: Springer, 2008.

Hall, Philip. Wave interactions in a three-dimensional attachment line boundary layer. Hampton, VA: NASA Langley Research Center, 1988.

C, Horstman K., i Ames Research Center, red. Intersecting shock-wave/turbulent boundary-layer interactions at Mach 8.3. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1992.

Center, Ames Research, red. Computation of three-dimensional shock wave and boundary-layer interactions. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1985.

C, Horstman K., i Ames Research Center, red. Intersecting shock-wave/turbulent boundary-layer interactions at Mach 8.3. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1992.

Center, Ames Research, red. Computation of three-dimensional shock wave and boundary-layer interactions. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1985.

Hall, Philip. On strongly nonlinear vortex/wave interactions in boundary-layer transition. Hampton, Va: Institute for Computer Applications in Science and Engineering, 1989.

C, Horstman K., i Ames Research Center, red. Intersecting shock-wave/turbulent boundary-layer interactions at Mach 8.3. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1992.

1948-, Smith F. T., i Langley Research Center, red. On strongly nonlinear vortex/wave interactions in boundary-layer transition. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

C, Horstman K., i Ames Research Center, red. Intersecting shock-wave/turbulent boundary-layer interactions at Mach 8.3. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1992.

United States. National Aeronautics and Space Administration., red. Observations of the magnetopause current layer: Cases with no boundary layer and tests of recent models. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

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.

Williams, K. E. The effect of varying Mach number on crossing, glancing shocks/turbulent boundary-layer interactions. Washington, D. C: AIAA, 1991.

S, Oran Elaine, Anderson John David i NASA Glenn Research Center, red. The interactions of a flame and its self-induced boundary layer. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

Coratekin, Turan. Numerical simulation of turbulent shock/boundary-layer interactions in hypersonic flows. Düsseldorf: VDI Verlag, 2000.

S, Oran Elaine, Anderson John David i NASA Glenn Research Center, red. The interactions of a flame and its self-induced boundary layer. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

1935-, Bradshaw P., i United States. National Aeronautics and Space Administration., red. Vortex/boundary-layer interactions, data report: Final report on NASA grant NAGw-581. London: Imperial College of Science and Technology, Dept. of Technology, 1988.

1935-, Bradshaw P., i United States. National Aeronautics and Space Administration., red. Vortex/boundary-layer interactions, data report: Final report on NASA grant NAGw-581. London: Imperial College of Science and Technology, Dept. of Technology, 1988.

Center, Ames Research, red. Turbulence modeling for sharp-fin-induced shock wave/turbulent boundary-layer interactions. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1990.

Boulder, University of Colorado, i United States. National Aeronautics and Space Administration., red. Wave/particle interactions in the plasma sheet. Boulder, Colo: University of Colorado, Boulder, 1985.

R, Krishnan. Mixed-layer and thermocline interactions associated with monsoonal forcing over the Arabian Sea. Pune: Indian Institute of Tropical Meteorology, 2004.

R, Krishnan. Mixed-layer and thermocline interactions associated with monsoonal forcing over the Arabian Sea. Pune: Indian Institute of Tropical Meteorology, 2004.

R, Krishnan. Mixed-layer and thermocline interactions associated with monsoonal forcing over the Arabian Sea. Pune: Indian Institute of Tropical Meteorology, 2004.

R, Krishnan. Mixed-layer and thermocline interactions associated with monsoonal forcing over the Arabian Sea. Pune: Indian Institute of Tropical Meteorology, 2004.

1935-, Bradshaw P., i United States. National Aeronautics and Space Administration., red. Vortex/boundary-layer interactions, data report: Final report on NASA grant NAGw-581 / A.D. Cutler and P. Bradshaw. London: Imperial College of Science and Technology, Department of Aeronautics, 1988.

Vermeulen, J. P. Parametric studies of shock wave/boundary layer interactions over 2D compression corners at Mach 6. Rhode Saint Genese, Belgium: von Karman Institute for Fluid Dynamics, 1992.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Special course on shock wave boundary layer interactions in supersonic and hypersonic flows. Neuilly-sur-Seine, France: AGARD, 1993.

Advisory Group for Aerospace Research and Development. Fluid Dynamics Panel. i Von Karman Institute for FluidDynamics., red. Special course on shock-wave/boundary-layer interactions in supersonic and hypersonic flows. Neuilly sur Seine: Agard, 1993.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Special course on shock-wave/boundary-layer interactions in supersonic and hypersonic flows. Neuilly-sur-Seine: AGARD, 1993.

United States. National Aeronautics and Space Administration., red. Vortex boundary-layer interactions, data report: Semiannual status report on research grant no. NAGW-581, period 1 March 1985 - 31 August 1985. London: Imperial College of Science and Technology, Department of Technology, 1985.

Bradshaw, P. Vortex boundary-layer interactions, data report: Semiannual status report on research grant no. NAGW-581, period 1 March 1985 - 31 August 1985. London: Imperial College of Science and Technology, Department of Technology, 1985.

Cui, Xuefeng. Interactions between climate and landcover changes on the Tibetan Plateau. Hamburg: University of Hamburg, 2009.

Hall, Philip. On the initial stages of vortex wave interactions in highly curved boundary layer flows. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

Hawboldt, R. J. Experimental study of shock wave and hypersonic boundary layer interactions near a convex corner. Downsview, Ont: University of Toronto, Institute for Aerospace Studies, 1993.

Hall, Philip. On the initial stages of vortex wave interactions in highly curved boundary layer flows. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

United States. National Aeronautics and Space Administration., red. Validation of the RPLUS3D code for supersonic inlet applications involving three-dimensional shock wave boundary layer interactions. [Washington, DC]: National Aeronautics and Space Administration, 1994.

United States. National Aeronautics and Space Administration., red. Validation of the RPLUS3D code for supersonic inlet applications involving three-dimensional shock wave boundary layer interactions. [Washington, DC]: National Aeronautics and Space Administration, 1994.