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1

Salacka, Thomas Francis. Review, implementation and test of the QAZID computational method with a view to wave rotor applications. Naval Postgraduate School, 1985.

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2

Ibragimov, Nail H. Selected works: Equivalence groups and invariants of differential equations. Extension of Euler's method to parabolic equations. Invariant and formal Lagrangians. Conservation law. ALGA Publications, 2009.

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3

United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., ed. Implicit methods for computing chemically reacting flow. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

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4

Huynh, Hung T. Accurate upwind methods for the Euler equations. National Aeronautics and Space Administration, 1993.

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5

Cockburn, B. The P¹-RKDG method for two-dimensional Euler equations of gas dynamics. National Aeronautics and Space Administration, Langley Research Center, 1991.

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6

Cockburn, B. The P¹-RKDG method for two-dimensional Euler equations of gas dynamics. National Aeronautics and Space Administration, Langley Research Center, 1991.

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7

Cockburn, B. The P¹-RKDG method for two-dimensional Euler equations of gas dynamics. National Aeronautics and Space Administration, Langley Research Center, 1991.

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8

Center, Lewis Research, ed. An efficient method for solving the steady Euler equations. National Aeronautics and Space Administration, Lewis Research Center, 1986.

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9

Center, Langley Research, ed. Canonical-variables multigrid method for steady-state Euler equation. National Aeronautics and Space Administration, Langley Research Center, 1994.

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10

Ta'asan, Shlomo. Canonical-variables multigrid method for steady-state Euler equations. Langley Research Center, 1994.

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11

Cockburn, Bernardo. The Pl-RKDG method for two-dimensional Euler equations of gas dynamics. Institute for Computer Applications in Science and Engineering, 1991.

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12

Smith, Ralph C. Numerical recovery of material parameters in Euler-Bernoulli beam models. Institute for Computer Applications in Science and Engineering, 1991.

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13

United States. National Aeronautics and Space Administration, ed. An LU-SSOR scheme for the Euler and Navier-Stokes equations. National Aeronautics and Space Administration, 1986.

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14

Yoon, Seokkwan. An LU-SSOR scheme for the Euler and Navier-Stokes equations. American Institute of Aeronautics and Astronautics, 1987.

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15

United States. National Aeronautics and Space Administration, ed. An LU-SSOR scheme for the Euler and Navier-Stokes equations. National Aeronautics and Space Administration, 1986.

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16

United States. National Aeronautics and Space Administration., ed. An LU-SSOR scheme for the Euler and Navier-Stokes equations. National Aeronautics and Space Administration, 1986.

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17

Lee, Dong-Ho. An efficient method to calculate rotor flow in hover & forward flight. American Institute of Aeronautics and Astronautics, 1993.

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18

Dang, T. Q. An Euler correction method for two and three-dimensional transonic flows. AIAA, 1987.

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19

Smith, Ralph C. A fully Sinc-Galerkin method for Euler-Bernoulli beam models. Institute for Computer Applications in Science and Engineering, 1990.

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20

Smith, Ralph C. A fully Sinc-Galerkin method for Euler-Bernoulli beam models. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1990.

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21

L, Bowers Kenneth, Lund J, Langley Research Center, and Institute for Computer Applications in Science and Engineering., eds. A fully Sinc-Galerkin method for Euler-Bernoulli beam models. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1990.

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22

E, Turkel, and Langley Research Center, eds. Multistage schemes with multigrid for Euler and Navier-Stokes equations: Components and analysis. National Aeronautics and Space Administration, Langley Research Center, 1997.

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23

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

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24

Toro, E. F. Random-choice based hybrid methods for one and two dimensional gas dynamics. College of Aeronautics, Cranfield Institute of Technology, 1988.

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25

INRIA Workshop on Numerical Methods for the Euler Equations of Fluid Dynamics (1983 Rocquencourt, Yvelines, France). Numerical methods for the Euler equations of fluid dynamics. Society for Industrial and Applied Mathematics, 1985.

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26

Harold, Atkins, Keyes David, and Langley Research Center, eds. Parallel implementation of the discontinuous Galerkin method. National Aeronautics and Space Administration, Langley Research Center, 1999.

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27

Iollo, Angelo. Pseudo-time method for optimal shape design using the Euler equations. Institute for Computer Applications in Science and Engineering, 1995.

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28

Iollo, Angelo. Shape optimization governed by the Euler equations using an adjoint method. Institute for Computer Applications in Science and Engineering, 1993.

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29

Roberts, Thomas W. Solution method for a hovering helicopter rotor using the Euler equations. American Institute of Aeronautics and Astronautics, 1985.

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30

Geojoe, Kuruvila, Ta'asan Shlomo, and Institute for Computer Applications in Science and Engineering., eds. Pseudo-time method for optimal shape design using the Euler equations. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1995.

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31

Geojoe, Kuruvila, Ta'asan Shlomo, and Institute for Computer Applications in Science and Engineering., eds. Pseudo-time method for optimal shape design using the Euler equations. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1995.

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32

Geojoe, Kuruvila, Ta'asan Shlomo, and Institute for Computer Applications in Science and Engineering., eds. Pseudo-time method for optimal shape design using the Euler equations. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1995.

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33

Manna, M. A three dimensional high resolution upwind finite volume Euler solver. Von Karman Institute for Fluid Dynamics, 1992.

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34

Perthame, B. On positivity preserving finite volume schemes for compressible Euler equations. Institute for Computer Applications in Science and Engineering, 1993.

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35

Schonfeld, Thilo. Methods to enhance the accuracy of finite volume schemes II. Aeronautical Research Institute of Sweden, 1991.

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36

Turkel, Eli. Accuracy of schemes for the Euler equations with non-uniform meshes. ICASE, 1985.

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37

Center, Langley Research, ed. Three dimensional unstructured multigrid for the Euler equations. National Aeronautics and Space Administration, Langley Research Center, 1991.

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38

J, Mavriplis D., and Langley Research Center, eds. Agglomeration multigrid for the three-dimensional Euler equations. National Aeronautics and Space Administration, Langley Research Center, 1994.

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39

Mavriplis, Dimitri J. Three dimensional unstructured multigrid for the Euler equations. ICASE, 1991.

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40

Cannizzaro, Frank E. A multiblock multigrid three-dimensional Euler equation solver. [s.n.], 1991.

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41

T, Batina John, Yang T. Y, and Langley Research Center, eds. Three-dimensional time-marching aeroelastic analyses using an unstructured-grid Euler method. National Aeronautics and Space Administration, Langley Research Center, 1992.

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42

T, Batina John, Yang T. Y, and Langley Research Center, eds. Three-dimensional time-marching aeroelastic analyses using an unstructured-grid Euler method. National Aeronautics and Space Administration, Langley Research Center, 1992.

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43

Iollo, Angelo. Shape optimization governed by the Euler equations using an adjoint method [microform]. National Aeronautics and Space Administration, Langley Research Center, 1993.

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44

T, Batina John, Yang T. Y, and Langley Research Center, eds. Three-dimensional time-marching aeroelastic analyses using an unstructured-grid Euler method. National Aeronautics and Space Administration, Langley Research Center, 1992.

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45

Anderson, W. Kyle. Grid generation and flow solution method for Euler equations on unstructured grids. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

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46

Blanco, Max. An implicit solution method for the Euler equations on unstructured triangular grids. National Library of Canada, 1995.

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47

Cai, Wei. Uniform high order spectral methods for one and two dimensional Euler equations. Institute for Computer Applications in Science and Engineering, 1991.

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48

Sidilkover, David. A genuinely multidimensional upwind scheme and efficient multigrid solver for the compressible Euler equations. Institute for Computer Applications in Science and Engineering, 1994.

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49

Mavriplis, Dimitri J. Accurate multigrid solution of the Euler equations on unstructured and adaptive meshes. ICASE, 1988.

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50

Löhner, Rainald. Finite element flux-corrected transport (FEM-FCT) for the Euler and Navier-Stokes equations. ICASE, 1987.

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