Bücher zum Thema „Turbulent shear layers“
Geben Sie eine Quelle nach APA, MLA, Chicago, Harvard und anderen Zitierweisen an
Machen Sie sich mit Top-50 Bücher für die Forschung zum Thema "Turbulent shear layers" bekannt.
Neben jedem Werk im Literaturverzeichnis ist die Option "Zur Bibliographie hinzufügen" verfügbar. Nutzen Sie sie, wird Ihre bibliographische Angabe des gewählten Werkes nach der nötigen Zitierweise (APA, MLA, Harvard, Chicago, Vancouver usw.) automatisch gestaltet.
Sie können auch den vollen Text der wissenschaftlichen Publikation im PDF-Format herunterladen und eine Online-Annotation der Arbeit lesen, wenn die relevanten Parameter in den Metadaten verfügbar sind.
Sehen Sie die Bücher für verschiedene Spezialgebieten durch und erstellen Sie Ihre Bibliographie auf korrekte Weise.
Smits, Alexander J. Turbulent shear layers in supersonic flow. 2. Aufl. New York: Springer, 2011.
Den vollen Inhalt der Quelle findenJean-Paul, Dussauge, Hrsg. Turbulent shear layers in supersonic flow. 2. Aufl. New York: Springer, 2006.
Den vollen Inhalt der Quelle findenJean-Paul, Dussauge, Hrsg. Turbulent shear layers in supersonic flow. Woodbury, N.Y: American Institute of Physics, 1996.
Den vollen Inhalt der Quelle findenPapamoschou, Dimitri. Structure of the compressible turbulent shear layer. Washington, D. C: American Institute of Aeronautics and Astronautics, 1989.
Den vollen Inhalt der Quelle findenY, Chen J., Limley J. L und Lewis Research Center. Institute for Computational Mechanics in Propulsion., Hrsg. Second order modeling of boundary-free turbulent shear flows. Cleveland, Ohio: NASA Lewis Research Center, Institute for Computational Mechanics in Propulsion, 1991.
Den vollen Inhalt der Quelle findenShau, Y. R. Experimental study of spreading rate enhancement of high Mach number turbulent shear layers. Washington, D. C: American Institute of Aeronautics and Astronautics, 1989.
Den vollen Inhalt der Quelle findenCenter, Ames Research, Hrsg. Improved two-equation k - [omega] turbulence models for aerodynamic flows. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1992.
Den vollen Inhalt der Quelle findenCenter, Ames Research, Hrsg. Improved two-equation k - [omega] turbulence models for aerodynamic flows. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1992.
Den vollen Inhalt der Quelle findenAdair, Desmond. Characteristics of merging shear layers and turbulent wakes of a multi-element airfoil. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1988.
Den vollen Inhalt der Quelle findenBrown, Douglas L. Computation of turbulent boundary layers employing the defect wall-function method. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.
Den vollen Inhalt der Quelle findenC, Dudek Julianne, Tierney Thomas P und United States. National Aeronautics and Space Administration., Hrsg. Grid resolution and turbulent inflow boundary condition recommendations for NPARC calculations. [Washington, DC]: National Aeronautics and Space Administration, 1995.
Den vollen Inhalt der Quelle findenF, Durst, und International Symposium on Turbulent Shear Flows, (9th : 1993 : Kyoto, Japan), Hrsg. Turbulent shear flows 9: Selected papers from the Ninth International Symposium on Turbulent Shear Flows, Kyoto, Japan, August 16-18, 1993. Berlin: Springer-Verlag, 1995.
Den vollen Inhalt der Quelle findenUniversity), International Symposium on Turbulent Shear Flows (7th 1989 Stanford. Turbulent shear flows 7: Selected papers from the Seventh International Symposium on Turbulent Shear Flows, Stanford University, USA, August 21-23, 1989. Berlin: Springer-Verlag, 1991.
Den vollen Inhalt der Quelle findenDélery, J., Hrsg. Turbulent Shear-Layer/Shock-Wave Interactions. Berlin, Heidelberg: Springer Berlin Heidelberg, 1986. http://dx.doi.org/10.1007/978-3-642-82770-9.
Der volle Inhalt der QuelleIUTAM Symposium (1985 Palaiseau, France). Turbulent shear-layer/shock-wave interactions. Herausgegeben von Délery J. 1939-, International Union of Theoretical and Applied Mechanics. und France. Office national d'études et de recherches aérospatiales. Berlin: Springer-Verlag, 1986.
Den vollen Inhalt der Quelle findenInternational Symposium on Turbulent Shear Flows (5th 1985 Cornell University, Ithaca, N.Y.). Turbulent shear flows: Papers from the Fifth International Symposium on Turbulent Shear Flows, August 7-9, 1985, Cornell University, Ithaca, NY. [University Park, Pa: Pennsylvania State University, 1985.
Den vollen Inhalt der Quelle findenWoppowa, Stefan. Über Gedächtniseffekte in der Turbulenz. Köln: Deutsche Forschungsanstalt für Luft- und Raumfahrt, 1993.
Den vollen Inhalt der Quelle findenAmerican Society of Mechanical Engineers. Winter Meeting. Shear flow: Structure interaction phenomena. New York, N.Y. (345 E. 47th St., New York): American Society of Mechanical Engineers, 1985.
Den vollen Inhalt der Quelle findenKim, S. W. Calculation of reattaching shear layers in divergent channel with a multiple-time-scale turbulence model. Cleveland, Ohio: Institute for Computational Mechanics in Propulusion, 1989.
Den vollen Inhalt der Quelle findenB, Gatski T., und Langley Research Center, Hrsg. An alternative assessment of second order closure models in turbulent shear flows. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1994.
Den vollen Inhalt der Quelle findenDriver, David M. Experimental study of a three-dimensional shear-driven turbulent boundary layer with streamwise adverse pressure gradient. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1990.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration., Hrsg. Turbulence modeling of free shear layers for high performance aircraft. San Jose, CA: MCAT Institute, 1993.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration., Hrsg. Turbulence modeling of free shear layers for high performance aircraft. San Jose, CA: MCAT Institute, 1993.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration., Hrsg. Turbulence modeling of free shear layers for high-performance aircraft. San Jose, CA: MCAT Institute, 1993.
Den vollen Inhalt der Quelle findenInternational Symposium on Turbulent Shear Flows (9th 1993 Kyoto, Japan). Turbulent shear flows 9: Selected papers from the Ninth International Symposium on Turbulent Shear Flows, Kyoto, Japan, August 16-18, 1993. Herausgegeben von Durst F. Berlin: Springer-Verlag, 1995.
Den vollen Inhalt der Quelle findenInternational Symposium on Turbulent Shear Flows (8th 1991 Munich, Germany). Turbulent shear flows 8: Selected papers from the Eighth International Symposium on Turbulent Shear Flows, Munich, FRG, September 9-11, 1991. Herausgegeben von Durst F. Berlin: Springer-Verlag, 1993.
Den vollen Inhalt der Quelle findenL, Bowles Roland, und Langley Research Center, Hrsg. A simple, analytic 3-dimensional downburst model based on boundary layer stagnation flow. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.
Den vollen Inhalt der Quelle findenL, Bowles Roland, und Langley Research Center, Hrsg. A simple, analytic 3-dimensional downburst model based on boundary layer stagnation flow. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.
Den vollen Inhalt der Quelle findenG, Huang P., MacInnes J. M und United States. National Aeronautics and Space Administration., Hrsg. Mesh refinement in a two-dimensional large eddy simulation of a forced shear layer. [Washington, DC]: National Aeronautics and Space Administration, 1989.
Den vollen Inhalt der Quelle findenSarkar, Sutanu. Application of a Reynolds stress turbulence model to the compressible shear layer. Hampton, Va: Institute for Computer Applications in Science and Engineering, 1990.
Den vollen Inhalt der Quelle findenDriver, David M. Experimental study of a three-dimensional, shear-driven, turbulent boundary layer using a three-dimensional laser doppler velocimeter. [New York]: American Institute of Aeronautics and Astronautics, 1985.
Den vollen Inhalt der Quelle findenDélery, J. Turbulent Shear-Layer/Shock-Wave Interactions: IUTAM Symposium, Palaiseau, France September 9-12, 1985. Berlin, Heidelberg: Springer Berlin Heidelberg, 1986.
Den vollen Inhalt der Quelle findenSarkar, Sarben. Application of a Reynolds stress turbulence model to the compressible shear layer. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.
Den vollen Inhalt der Quelle findenIUTAM Symposium (1993 Potsdam, N.Y.). Nonlinear instability of nonparallel flows. Berlin: Springer-Verlag, 1994.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration., Hrsg. Low re multiple-time-scale turbulence model and calculations of steady and pulsating shear layers. [Washington, DC]: National Aeronautics and Space Administration, 1992.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration., Hrsg. Low re multiple-time-scale turbulence model and calculations of steady and pulsating shear layers. [Washington, DC]: National Aeronautics and Space Administration, 1992.
Den vollen Inhalt der Quelle findenM, Abbott John, und United States. National Aeronautics and Space Administration., Hrsg. Control of flow separation and mixing by aerodynamic excitation. [Washington, D.C.]: NASA, 1990.
Den vollen Inhalt der Quelle findenM, Abbott John, und United States. National Aeronautics and Space Administration., Hrsg. Control of flow separation and mixing by aerodynamic excitation. [Washington, D.C.]: NASA, 1990.
Den vollen Inhalt der Quelle findenC, Yee H., und Research Institute for Advanced Computer Science (U.S.), Hrsg. Performance of low dissipative high order shock-capturing schemes for shock-turbulence interactions. [Moffett Field, Calif.]: Research Institute for Advanced Computer Science, NASA Ames Research Center, 1998.
Den vollen Inhalt der Quelle findenKline, Stephen. The physics of turbulence in the boundary layer: Final report ... NASA grant NAG-1-1610. [Washington, DC: National Aeronautics and Space Administration, 1996.
Den vollen Inhalt der Quelle findenClawson, K. L. Meteorological measurements during the urban 2000/VTMX field study. Silver Spring, Md: U.S. Dept. of Commerce, National Oceanic and Atmospheric Administration, Oceanic and Atmospheric Research Laboratories, Air Resources Laboratory, 2002.
Den vollen Inhalt der Quelle findenT, Chang C., und United States. National Aeronautics and Space Administration., Hrsg. Turbulence measurement in a reacting and non-reacting shear layer at a high subsonic Mach number. [Washington, DC]: National Aeronautics and Space Administration, 1993.
Den vollen Inhalt der Quelle findenT, Chang C., und United States. National Aeronautics and Space Administration., Hrsg. Turbulence measurement in a reacting and non-reacting shear layer at a high subsonic Mach number. [Washington, DC]: National Aeronautics and Space Administration, 1993.
Den vollen Inhalt der Quelle findenKamada, Ray. Amending the w* velocity scale for surface layer, entrainment zone, and baroclinic shear in mixed forced/free turbulent convection. Monterey, Calif: Naval Postgraduate School, 1992.
Den vollen Inhalt der Quelle findenDahl, M. D. Noise from supersonic coaxial jets. [Washington, DC: National Aeronautics and Space Administration, 1997.
Den vollen Inhalt der Quelle findenDahl, M. D. Noise from supersonic coaxial jets. [Washington, DC: National Aeronautics and Space Administration, 1997.
Den vollen Inhalt der Quelle findenJ, Morris P., und United States. National Aeronautics and Space Administration., Hrsg. Noise from supersonic coaxial jets. [Washington, DC: National Aeronautics and Space Administration, 1997.
Den vollen Inhalt der Quelle findenDahl, M. D. Noise from supersonic coaxial jets. [Washington, DC: National Aeronautics and Space Administration, 1997.
Den vollen Inhalt der Quelle findenDahl, M. D. Noise from supersonic coaxial jets. [Washington, DC: National Aeronautics and Space Administration, 1997.
Den vollen Inhalt der Quelle findenJ, Morris P., und United States. National Aeronautics and Space Administration., Hrsg. Noise from supersonic coaxial jets. [Washington, DC: National Aeronautics and Space Administration, 1997.
Den vollen Inhalt der Quelle finden