Książki na temat „Inviscid Compressible Fluid Flows”

United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., red. 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.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., red. 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.

E, Jorgenson Philip C., i United States. National Aeronautics and Space Administration., red. A mixed volume grid approach for the Euler and Navier-Stokes equations. [Washington, DC]: National Aeronautics and Space Administration, 1996.

E, Jorgenson Philip C., i United States. National Aeronautics and Space Administration., red. A mixed volume grid approach for the Euler and Navier-Stokes equations. [Washington, DC]: National Aeronautics and Space Administration, 1996.

E, Grosch C., i Institute for Computer Applications in Science and Engineering., red. Inviscid spatial stability of a compressible mixing layer. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1989.

Feireisl, Eduard, Mária Lukáčová-Medviďová, Hana Mizerová i Bangwei She. Numerical Analysis of Compressible Fluid Flows. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-73788-7.

Center, Langley Research, red. Canonical forms of multidimensional steady inviscid flows. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

Institute for Computer Applications in Science and Engineering., red. Krylov methods for compressible flows. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1995.

Krainer, Andreas. Viscous-inviscid interaction analysis of incompressible cascade flows. Monterey, Calif: Naval Postgraduate School, 1986.

Tuncer, Cebeci, red. Computational fluid dynamics for engineers: From panel to Navier-Stokes methods with computer programs. Long Beach, Calif: Horizons Pub. Inc., 2005.

Kentfield, John A. C. Nonsteady, one-dimensional, internal, compressible flows: Theory and applications. New York: Oxford University Press, 1993.

Reddy, K. C. Finite element solver for 3-D compressible viscous flows. [Washington, DC: National Aeronautics and Space Administration, 1987.

Maestrello, Lucio. Active control of compressible flows on a curved surface. Hampton, Va: ICASE, 1985.

Moro, Boris. Analysis of certain inviscid flows on the beta plane. Woods Hole, Mass: Woods Hole Oceanographic Institution, c1986., 1986.

Deshpande, Suresh M. A second-order accurate kinetic-theory-based method for inviscid compressible flows. Hampton, Va: Langley Research Center, 1986.

Reddy, 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.

H, Klopfer Goetz, Montagne J. -L i Ames Research Center, red. High-resolution shock-capturing schemes for inviscid and viscous hypersonic flows. Moffet Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1988.

H, Klopfer Goetz, Montagne J. -L i Ames Research Center, red. High-resolution shock-capturing schemes for inviscid and viscous hypersonic flows. Moffet Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1988.

H, Klopfer Goetz, Montagne J. -L i Ames Research Center, red. High-resolution shock-capturing schemes for inviscid and viscous hypersonic flows. Moffet Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1988.

Fix, 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.

Manil, Suri, Institute for Computer Applications in Science and Engineering. i Langley Research Center, red. Three-dimensional mass conserving elements for compressible flows. Hampton, Va: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1985.

United States. National Aeronautics and Space Administration., red. Near-wall modelling of compressible turbulent flows. Tempe, Ariz: College of Engineering & Applied Science, Arizona State University, 1991.

United States. National Aeronautics and Space Administration., red. Studies of pressure-velocity coupling schemes for analysis of incompressible and compressible flows. [Washington, D.C.?: National Aeronautics and Space Administration, 1987.

Ishiguro, Tomiko. Numerical analysis of inviscid compressible flows about wing- fuselage combinations based on the Euler equations. Chofu, Tokyo, Japan: National Aerospace Laboratory, 1986.

GAMM 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.

Tsang, Kalvin C. H. Parallel implicit Newton-Krylov-Schwarz method for predicting compressible turbomachinery flows. [Downsview, Ont.]: University of Toronto, Institute for Aerospace Studies, 2003.

Odile, Bristeau Marie, i GAMM Workshop on Numerical Simulation of Compressible Navier-Stokes Flows (1985 : Nice, France), red. Numerical simulation of compressible Navier-Stokes flows: A GAMM workshop. Braunschweig: F. Vieweg, 1987.

Gnoffo, 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.

Gnoffo, Peter A. An upwind-biased, point-implicit relaxation algorithm for viscous, compressible perfect-gas flows. Hampton, Va: Langley Research Center, 1990.

Gnoffo, 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.

Kopriva, David A. A conservative staggered-grid Chebyshev multidomain method for compressible flows. Hampton, Va: Langley Research Center, 1995.

Center, Langley Research, red. A conservative staggered-grid chebyshev multidomain method for compressible flows. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

Coirier, William J. Solution-adaptive Cartesian cell approach for viscous and inviscid flows. Washington, DC: American Institute of Aeronautics and Astronautics, 1996.

Coirier, William J. Solution-adaptive Cartesian cell approach for viscous and inviscid flows. Washington, DC: American Institute of Aeronautics and Astronautics, 1996.

Coirier, William J. Solution-adaptive Cartesian cell approach for viscous and inviscid flows. Washington, DC: American Institute of Aeronautics and Astronautics, 1996.

Coirier, William J. Solution-adaptive Cartesian cell approach for viscous and inviscid flows. Washington, DC: American Institute of Aeronautics and Astronautics, 1996.

Scott, James R. Compressible flows with periodic vortical disturbances around lifting airfoils. [Cleveland, Ohio: Lewis Research Center, 1991.

United States. National Aeronautics and Space Administration., red. 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.

Development, 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.

North 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.

Institute for Computer Applications in Science and Engineering., red. 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.

N, Vatsa V., Radespiel R i Institute for Computer Applications in Science and Engineering., red. Preconditioning methods for low-speed flows. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1996.

Liu, Jianguo. A high order discontinuous Galerkin method for 2D incompressible flows. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

University, Arizona State, i Langley Research Center, red. Near-wall modelling of compressible turbulent flows: A semi-annual progress report. Tempe, Ariz: Arizona State University, 1990.

United States. National Aeronautics and Space Administration., red. Near-wall modelling of compressible turbulent flows: A semi-annual progress report. Tempe, Ariz: College of Engineering & Applied Sciences, Arizona State University, 1991.

United States. National Aeronautics and Space Administration., red. Near-wall modelling of compressible turbulent flows: A semi-annual progress report. Tempe, Ariz: College of Engineering & Applied Sciences, Arizona State University, 1991.

United States. National Aeronautics and Space Administration., red. Small-amplitude disturbances in turbomachine flows with swirl. [Washington, DC: National Aeronautics and Space Administration, 1994.

United States. National Aeronautics and Space Administration., red. Small-amplitude disturbances in turbomachine flows with swirl. [Washington, DC: National Aeronautics and Space Administration, 1994.

Institute for Computer Applications in Science and Engineering., red. 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.

D, Modiano, Colella P i United States. National Aeronautics and Space Administration., red. Computations of unsteady viscous compressible flows using adaptive mesh refinement in curvilinear body-fitted grid systems. [Washington, DC]: National Aeronautics and Space Administration, 1994.