Livres sur le sujet « High Resolution Shock Capturing »
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1934-, Jameson Antony, et United States. National Aeronautics and Space Administration, dir. High-resolution shock capturing scheme for high Mach number internal flow. [Washington, D.C.] : National Aeronautics and Space Administration, 1986.
Trouver le texte intégral1934-, Jameson Antony, et United States. National Aeronautics and Space Administration, dir. High-resolution shock capturing scheme for high Mach number internal flow. [Washington, D.C.] : National Aeronautics and Space Administration, 1986.
Trouver le texte intégralCenter, Ames Research, dir. Numerical experiments with a symmetric high-resolution shock-capturing scheme. Moffett Field, Calif : National Aeronautics and Space Administration, Ames Research Center, 1986.
Trouver le texte intégralCenter, Ames Research, dir. A class of high-resolution explicit and implicit shock-capturing methods. Moffett Field, Calif : National Aeronautics and Space Administration, Ames Research Center, 1989.
Trouver le texte intégralCenter, Ames Research, dir. A class of high-resolution explicit and implicit shock-capturing methods. Moffett Field, Calif : National Aeronautics and Space Administration, Ames Research Center, 1989.
Trouver le texte intégralCenter, Ames Research, dir. A class of high-resolution explicit and implicit shock-capturing methods. Moffett Field, Calif : National Aeronautics and Space Administration, Ames Research Center, 1989.
Trouver le texte intégralH, Klopfer Goetz, Montagne J. -L et Ames Research Center, dir. High-resolution shock-capturing schemes for inviscid and viscous hypersonic flows. Moffet Field, Calif : National Aeronautics and Space Administration, Ames Research Center, 1988.
Trouver le texte intégralH, Klopfer Goetz, Montagne J. -L et Ames Research Center, dir. High-resolution shock-capturing schemes for inviscid and viscous hypersonic flows. Moffet Field, Calif : National Aeronautics and Space Administration, Ames Research Center, 1988.
Trouver le texte intégralH, Klopfer Goetz, Montagne J. -L et Ames Research Center, dir. High-resolution shock-capturing schemes for inviscid and viscous hypersonic flows. Moffet Field, Calif : National Aeronautics and Space Administration, Ames Research Center, 1988.
Trouver le texte intégralC, Yee Henry, Vinokur Marcel et Ames Research Center, dir. Comparative study of high-resolution shock-capturinng schemes for a real gas. Moffett Field, Calif : National Aeronautics and Space Administration, Ames Research Center, 1987.
Trouver le texte intégralC, Yee H., et Research Institute for Advanced Computer Science (U.S.), dir. 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.
Trouver le texte intégralGustafsson, Bertil. High-order centered difference methods with sharp shock resolution. [Moffett Field, Calif.] : Research Institute for Advanced Computer Science, NASA Ames Research Center, 1994.
Trouver le texte intégralBertil, Gustafsson. High-order centered difference methods with sharp shock resolution. [Moffett Field, Calif.] : Research Institute for Advanced Computer Science, NASA Ames Research Center, 1994.
Trouver le texte intégralGustafsson, Bertil. High-order centered difference methods with sharp shock resolution. [Moffett Field, Calif.] : Research Institute for Advanced Computer Science, NASA Ames Research Center, 1994.
Trouver le texte intégralW, Jerome Joseph, Osher Stanley et Langley Research Center, dir. Solution of the hydrodynamic device model using high-order non-oscillatory shock capturing algorithms. Hampton, Va : National Aeronautics and Space Administration, Langley Research Center, 1989.
Trouver le texte intégralUnited States. National Aeronautics and Space Administration., dir. Performance Of Low Dissipative High Order Shock-Capturing Schemes For Shock-Turbulence... NASA/CR-1998-208354... Aug. 6, 1998. [S.l : s.n., 1999.
Trouver le texte intégralGroth, Clinton P. T. TVD flux-difference split methods for high-speed thermochemical nonequilibrium flows with strong shocks. [Toronto, Ont.] : University of Toronto, Graduate Dept. of Aerospace Science and Engineering, 1993.
Trouver le texte intégralGroth, Clinton P. T. TVD flux-difference split methods for high-speed thermochemical equilibrium flows with strong shocks. [Downsview, Ont.] : University of Toronto, Institute for Aerospace Studies, 1993.
Trouver le texte intégralUnited States. National Aeronautics and Space Administration., dir. Low Dissipative High Order Shock-Capturing Methods Using Characteristic-Based Filters... NASA/CR-1998-208350... Aug. 6, 1998. [S.l : s.n., 1999.
Trouver le texte intégralXiao-Yen, Wang, Chow Chuen-Yen 1932-, Lewis Research Center et United States. National Aeronautics and Space Administration., dir. The space-time conservation element and solution element method--a new high-resolution and genuinely multidimensional paradigm for solving conservation laws. [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, 1998.
Trouver le texte intégralXiao-Yen, Wang, Chow Chuen-Yen 1932-, Lewis Research Center et United States. National Aeronautics and Space Administration., dir. The space-time conservation element and solution element method--a new high-resolution and genuinely multidimensional paradigm for solving conservation laws. [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, 1998.
Trouver le texte intégralXiao-Yen, Wang, Chow Chuen-Yen 1932-, Lewis Research Center et United States. National Aeronautics and Space Administration., dir. The space-time conservation element and solution element method--a new high-resolution and genuinely multidimensional paradigm for solving conservation laws. [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, 1998.
Trouver le texte intégralXiao-Yen, Wang, Chow Chuen-Yen 1932- et Lewis Research Center, dir. The space-time conservation element and solution element method--a new high-resolution and genuinely multidimensional paradigm for solving conservation laws. [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, 1998.
Trouver le texte intégral1932-, Chow Chuen-Yen, Chang Sin-Chung et Lewis Research Center, dir. The space-time conservation element and solution element method--a new high-resolution and genuinely multidimensional paradigm for solving conservation laws. [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, 1998.
Trouver le texte intégral1932-, Chow Chuen-Yen, Chang Sin-Chung, Lewis Research Center et United States. National Aeronautics and Space Administration., dir. The space-time conservation element and solution element method--a new high-resolution and genuinely multidimensional paradigm for solving conservation laws. [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, 1998.
Trouver le texte intégralHigh-resolution shock capturing scheme for high Mach number internal flow. [Washington, D.C.] : National Aeronautics and Space Administration, 1986.
Trouver le texte intégralHigh-resolution shock capturing scheme for high Mach number internal flow. [Washington, D.C.] : National Aeronautics and Space Administration, 1986.
Trouver le texte intégralNational Aeronautics and Space Administration (NASA) Staff. High-Resolution Shock-Capturing Schemes for Inviscid and Viscous Hypersonic Flows. Independently Published, 2018.
Trouver le texte intégralLow dissipative high order shock-capturing methods using characteristic-based filters. [Moffett Field, Calif.] : Research Institute for Advanced Computer Science, NASA Ames Research Center, 1998.
Trouver le texte intégralExplicit and implicit compact high-resolution shock-capturing methods for multidimensional Euler equations I, formulation. Moffett Field, Calif : National Aeronautics and Space Administration, Ames Research Center, 1995.
Trouver le texte intégralGlaubitz, Jan. Shock Capturing and High-Order Methods for Hyperbolic Conservation Laws. Logos Verlag Berlin, 2020.
Trouver le texte intégralNational Aeronautics and Space Administration (NASA) Staff. High-Order Centered Difference Methods with Sharp Shock Resolution. Independently Published, 2018.
Trouver le texte intégralNational Aeronautics and Space Administration (NASA) Staff. Solution of the Hydrodynamic Device Model Using High-Order Non-Oscillatory Shock Capturing Algorithms. Independently Published, 2018.
Trouver le texte intégralNational Aeronautics and Space Administration (NASA) Staff. High Order Finite Difference Scheme with Sharp Shock Resolution for the Euler Equations. Independently Published, 2018.
Trouver le texte intégralGroth, Clinton P. T. TVD flux-difference split methods for high-speed thermochemical nonequilibrium flows with strong shocks. 1993.
Trouver le texte intégralThe space-time conservation element and solution element method--a new high-resolution and genuinely multidimensional paradigm for solving conservation laws. [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, 1998.
Trouver le texte intégralThe space-time conservation element and solution element method--a new high-resolution and genuinely multidimensional paradigm for solving conservation laws. [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, 1998.
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