Книги з теми "Inviscid Compressible Fluid Flows"
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United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., ed. A second-order accurate kinetic-theory-based method for inviscid compressible flows. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., ed. A second-order accurate kinetic-theory-based method for inviscid compressible flows. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.
Знайти повний текст джерелаE, Jorgenson Philip C., and United States. National Aeronautics and Space Administration., eds. A mixed volume grid approach for the Euler and Navier-Stokes equations. [Washington, DC]: National Aeronautics and Space Administration, 1996.
Знайти повний текст джерелаE, Jorgenson Philip C., and United States. National Aeronautics and Space Administration., eds. A mixed volume grid approach for the Euler and Navier-Stokes equations. [Washington, DC]: National Aeronautics and Space Administration, 1996.
Знайти повний текст джерелаE, Grosch C., and Institute for Computer Applications in Science and Engineering., eds. Inviscid spatial stability of a compressible mixing layer. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1989.
Знайти повний текст джерелаFeireisl, Eduard, Mária Lukáčová-Medviďová, Hana Mizerová, and Bangwei She. Numerical Analysis of Compressible Fluid Flows. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-73788-7.
Повний текст джерелаCenter, Langley Research, ed. Canonical forms of multidimensional steady inviscid flows. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.
Знайти повний текст джерелаInstitute for Computer Applications in Science and Engineering., ed. Krylov methods for compressible flows. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1995.
Знайти повний текст джерелаKrainer, Andreas. Viscous-inviscid interaction analysis of incompressible cascade flows. Monterey, Calif: Naval Postgraduate School, 1986.
Знайти повний текст джерелаTuncer, Cebeci, ed. Computational fluid dynamics for engineers: From panel to Navier-Stokes methods with computer programs. Long Beach, Calif: Horizons Pub. Inc., 2005.
Знайти повний текст джерелаKentfield, John A. C. Nonsteady, one-dimensional, internal, compressible flows: Theory and applications. New York: Oxford University Press, 1993.
Знайти повний текст джерелаReddy, K. C. Finite element solver for 3-D compressible viscous flows. [Washington, DC: National Aeronautics and Space Administration, 1987.
Знайти повний текст джерелаMaestrello, Lucio. Active control of compressible flows on a curved surface. Hampton, Va: ICASE, 1985.
Знайти повний текст джерелаMoro, Boris. Analysis of certain inviscid flows on the beta plane. Woods Hole, Mass: Woods Hole Oceanographic Institution, c1986., 1986.
Знайти повний текст джерелаDeshpande, Suresh M. A second-order accurate kinetic-theory-based method for inviscid compressible flows. Hampton, Va: Langley Research Center, 1986.
Знайти повний текст джерелаReddy, K. C. A finite element solver for 3-D compressible viscous flows. [Huntsville], AL: National Aeronautics and Space Aadministration, MSFG, Marshall Space Flight Center, 1990.
Знайти повний текст джерелаH, Klopfer Goetz, Montagne J. -L, and Ames Research Center, eds. High-resolution shock-capturing schemes for inviscid and viscous hypersonic flows. Moffet Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1988.
Знайти повний текст джерелаH, Klopfer Goetz, Montagne J. -L, and Ames Research Center, eds. High-resolution shock-capturing schemes for inviscid and viscous hypersonic flows. Moffet Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1988.
Знайти повний текст джерелаH, Klopfer Goetz, Montagne J. -L, and Ames Research Center, eds. High-resolution shock-capturing schemes for inviscid and viscous hypersonic flows. Moffet Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1988.
Знайти повний текст джерелаFix, George J. Three-dimensional mass conserving elements for compressible flows. Hampton, Va: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1985.
Знайти повний текст джерелаManil, Suri, Institute for Computer Applications in Science and Engineering., and Langley Research Center, eds. Three-dimensional mass conserving elements for compressible flows. Hampton, Va: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1985.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Near-wall modelling of compressible turbulent flows. Tempe, Ariz: College of Engineering & Applied Science, Arizona State University, 1991.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Studies of pressure-velocity coupling schemes for analysis of incompressible and compressible flows. [Washington, D.C.?: National Aeronautics and Space Administration, 1987.
Знайти повний текст джерелаIshiguro, Tomiko. Numerical analysis of inviscid compressible flows about wing- fuselage combinations based on the Euler equations. Chofu, Tokyo, Japan: National Aerospace Laboratory, 1986.
Знайти повний текст джерелаGAMM Workshop on the Numerical Simulation of Compressible Euler Flows (1986 INRIA). Numerical simulation of compressible Euler flows: A GAMM Workshop. Braunschweig: Friedr. Vieweg & Sohn, 1989.
Знайти повний текст джерелаTsang, Kalvin C. H. Parallel implicit Newton-Krylov-Schwarz method for predicting compressible turbomachinery flows. [Downsview, Ont.]: University of Toronto, Institute for Aerospace Studies, 2003.
Знайти повний текст джерелаOdile, Bristeau Marie, and GAMM Workshop on Numerical Simulation of Compressible Navier-Stokes Flows (1985 : Nice, France), eds. Numerical simulation of compressible Navier-Stokes flows: A GAMM workshop. Braunschweig: F. Vieweg, 1987.
Знайти повний текст джерелаGnoffo, Peter A. An upwind-biased, point-implicit relaxation algorithm for viscous, compressible perfect-gas flows. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
Знайти повний текст джерелаGnoffo, Peter A. An upwind-biased, point-implicit relaxation algorithm for viscous, compressible perfect-gas flows. Hampton, Va: Langley Research Center, 1990.
Знайти повний текст джерелаGnoffo, Peter A. An upwind-biased, point-implicit relaxation algorithm for viscous, compressible perfect-gas flows. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
Знайти повний текст джерелаKopriva, David A. A conservative staggered-grid Chebyshev multidomain method for compressible flows. Hampton, Va: Langley Research Center, 1995.
Знайти повний текст джерелаCenter, Langley Research, ed. A conservative staggered-grid chebyshev multidomain method for compressible flows. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.
Знайти повний текст джерелаCoirier, William J. Solution-adaptive Cartesian cell approach for viscous and inviscid flows. Washington, DC: American Institute of Aeronautics and Astronautics, 1996.
Знайти повний текст джерелаCoirier, William J. Solution-adaptive Cartesian cell approach for viscous and inviscid flows. Washington, DC: American Institute of Aeronautics and Astronautics, 1996.
Знайти повний текст джерелаCoirier, William J. Solution-adaptive Cartesian cell approach for viscous and inviscid flows. Washington, DC: American Institute of Aeronautics and Astronautics, 1996.
Знайти повний текст джерелаCoirier, William J. Solution-adaptive Cartesian cell approach for viscous and inviscid flows. Washington, DC: American Institute of Aeronautics and Astronautics, 1996.
Знайти повний текст джерелаScott, James R. Compressible flows with periodic vortical disturbances around lifting airfoils. [Cleveland, Ohio: Lewis Research Center, 1991.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Computation technique for compressible vortex flows using the integral equation solution: Final report. Norfolk, Va: Dept. of Mechanical Engineering and Mechanics, College of Engineering, Old Dominion University, 1988.
Знайти повний текст джерелаDevelopment, North Atlantic Treaty Organization Advisory Group for Aerospace Research and. Round table discussion on modelling of time-variant flows using vortex dynamics. Neuilly sur Seine, France: AGARD, 1987.
Знайти повний текст джерелаNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Round Table Discussion on Modelling of Time-Variant Flows Using Vortex Dynamics. S.l: s.n, 1986.
Знайти повний текст джерелаInstitute for Computer Applications in Science and Engineering., ed. A Cartesian grid approach with hierarchical refinement for compressible flows. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1994.
Знайти повний текст джерелаN, Vatsa V., Radespiel R, and Institute for Computer Applications in Science and Engineering., eds. Preconditioning methods for low-speed flows. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1996.
Знайти повний текст джерелаLiu, Jianguo. A high order discontinuous Galerkin method for 2D incompressible flows. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.
Знайти повний текст джерелаUniversity, Arizona State, and Langley Research Center, eds. Near-wall modelling of compressible turbulent flows: A semi-annual progress report. Tempe, Ariz: Arizona State University, 1990.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Near-wall modelling of compressible turbulent flows: A semi-annual progress report. Tempe, Ariz: College of Engineering & Applied Sciences, Arizona State University, 1991.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Near-wall modelling of compressible turbulent flows: A semi-annual progress report. Tempe, Ariz: College of Engineering & Applied Sciences, Arizona State University, 1991.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Small-amplitude disturbances in turbomachine flows with swirl. [Washington, DC: National Aeronautics and Space Administration, 1994.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Small-amplitude disturbances in turbomachine flows with swirl. [Washington, DC: National Aeronautics and Space Administration, 1994.
Знайти повний текст джерелаInstitute for Computer Applications in Science and Engineering., ed. Some developments of the equilibrium particle simulation method for the direct simulation of compressible flows. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1995.
Знайти повний текст джерелаD, Modiano, Colella P, and United States. National Aeronautics and Space Administration., eds. Computations of unsteady viscous compressible flows using adaptive mesh refinement in curvilinear body-fitted grid systems. [Washington, DC]: National Aeronautics and Space Administration, 1994.
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