Books on the topic 'High Resolution Shock Capturing'

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1

1934-, Jameson Antony, and United States. National Aeronautics and Space Administration, eds. High-resolution shock capturing scheme for high Mach number internal flow. [Washington, D.C.]: National Aeronautics and Space Administration, 1986.

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2

1934-, Jameson Antony, and United States. National Aeronautics and Space Administration, eds. High-resolution shock capturing scheme for high Mach number internal flow. [Washington, D.C.]: National Aeronautics and Space Administration, 1986.

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3

Center, Ames Research, ed. Numerical experiments with a symmetric high-resolution shock-capturing scheme. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1986.

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4

Center, Ames Research, ed. A class of high-resolution explicit and implicit shock-capturing methods. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1989.

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5

Center, Ames Research, ed. A class of high-resolution explicit and implicit shock-capturing methods. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1989.

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6

Center, Ames Research, ed. A class of high-resolution explicit and implicit shock-capturing methods. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1989.

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7

H, 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.

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8

H, 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.

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9

H, 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.

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10

C, Yee Henry, Vinokur Marcel, and Ames Research Center, eds. Comparative study of high-resolution shock-capturinng schemes for a real gas. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1987.

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11

C, Yee H., and Research Institute for Advanced Computer Science (U.S.), eds. 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.

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12

Gustafsson, Bertil. High-order centered difference methods with sharp shock resolution. [Moffett Field, Calif.]: Research Institute for Advanced Computer Science, NASA Ames Research Center, 1994.

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13

Bertil, Gustafsson. High-order centered difference methods with sharp shock resolution. [Moffett Field, Calif.]: Research Institute for Advanced Computer Science, NASA Ames Research Center, 1994.

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14

Gustafsson, Bertil. High-order centered difference methods with sharp shock resolution. [Moffett Field, Calif.]: Research Institute for Advanced Computer Science, NASA Ames Research Center, 1994.

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15

W, Jerome Joseph, Osher Stanley, and Langley Research Center, eds. 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.

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16

United States. National Aeronautics and Space Administration., ed. Performance Of Low Dissipative High Order Shock-Capturing Schemes For Shock-Turbulence... NASA/CR-1998-208354... Aug. 6, 1998. [S.l: s.n., 1999.

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17

Groth, 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.

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18

Groth, 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.

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19

United States. National Aeronautics and Space Administration., ed. Low Dissipative High Order Shock-Capturing Methods Using Characteristic-Based Filters... NASA/CR-1998-208350... Aug. 6, 1998. [S.l: s.n., 1999.

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20

Xiao-Yen, Wang, Chow Chuen-Yen 1932-, Lewis Research Center, and United States. National Aeronautics and Space Administration., eds. 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.

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21

Xiao-Yen, Wang, Chow Chuen-Yen 1932-, Lewis Research Center, and United States. National Aeronautics and Space Administration., eds. 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.

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22

Xiao-Yen, Wang, Chow Chuen-Yen 1932-, Lewis Research Center, and United States. National Aeronautics and Space Administration., eds. 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.

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23

Xiao-Yen, Wang, Chow Chuen-Yen 1932-, and Lewis Research Center, eds. 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.

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24

1932-, Chow Chuen-Yen, Chang Sin-Chung, and Lewis Research Center, eds. 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.

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25

1932-, Chow Chuen-Yen, Chang Sin-Chung, Lewis Research Center, and United States. National Aeronautics and Space Administration., eds. 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.

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26

High-resolution shock capturing scheme for high Mach number internal flow. [Washington, D.C.]: National Aeronautics and Space Administration, 1986.

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27

High-resolution shock capturing scheme for high Mach number internal flow. [Washington, D.C.]: National Aeronautics and Space Administration, 1986.

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28

National Aeronautics and Space Administration (NASA) Staff. High-Resolution Shock-Capturing Schemes for Inviscid and Viscous Hypersonic Flows. Independently Published, 2018.

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29

Low dissipative high order shock-capturing methods using characteristic-based filters. [Moffett Field, Calif.]: Research Institute for Advanced Computer Science, NASA Ames Research Center, 1998.

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30

Explicit 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.

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31

Glaubitz, Jan. Shock Capturing and High-Order Methods for Hyperbolic Conservation Laws. Logos Verlag Berlin, 2020.

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32

National Aeronautics and Space Administration (NASA) Staff. High-Order Centered Difference Methods with Sharp Shock Resolution. Independently Published, 2018.

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33

National Aeronautics and Space Administration (NASA) Staff. Solution of the Hydrodynamic Device Model Using High-Order Non-Oscillatory Shock Capturing Algorithms. Independently Published, 2018.

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34

National Aeronautics and Space Administration (NASA) Staff. High Order Finite Difference Scheme with Sharp Shock Resolution for the Euler Equations. Independently Published, 2018.

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35

Groth, Clinton P. T. TVD flux-difference split methods for high-speed thermochemical nonequilibrium flows with strong shocks. 1993.

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36

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.

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37

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.

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