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1

Dannenhoffer, John F. Grid adaptation for the 2-D Euler equations. American Institute of Aeronautics and Astronautics, 1985.

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2

Predovic, D. Tom. Multigrid solution of the Euler equations using unstructured adaptive meshes. University of Toronto, Dept. of Aerospace Science and Engineering, 1994.

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3

Mavriplis, Dimitri J. Multigrid solution of the Euler equations on unstructured and adaptive meshes. ICASE, 1987.

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4

Djomehri, M. Jahed. An assessment of the adaptive unstructured tetrahedral grid, Euler flow solver code FELISA. Ames Research Center, 1994.

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5

Mavriplis, Dimitri J. Zonal multigrid solution of compressible flow problems on unstructured and adaptive meshes. ICASE, 1989.

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6

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

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7

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

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8

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

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9

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

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10

Coirier, William J. A Cartesian, cell-based approach for adaptively-refined solutions of the Euler and Navier-Stokes equations. National Aeronautics and Space Administration, 1994.

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11

Coirier, William J. An adaptively-refined, Cartesian cell-based scheme for the Euler and Navier-Stokes equations. National Aeronautics and Space Administration, 1994.

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12

Shapiro, Richard A. Adaptive finite element solution algorithm for the Euler equations. Vieweg, 1991.

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13

Shapiro, Richard A., ed. Adaptive Finite Element Solution Algorithm for the Euler Equations. Vieweg+Teubner Verlag, 1991. http://dx.doi.org/10.1007/978-3-322-87879-3.

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14

Wehner, Edward. A Newton-Krylov solver for the euler equations on unstructured grids. Deartment of Aerospace Science and Engineering, University of Toronto, 2001.

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15

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

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16

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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17

Mavriplis, Dimitri J. Multigrid solution of the two-dimensional Euler equations on unstructured triangular meshes. American Institute of Aeronautics and Astronautics, 1987.

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18

Belk, Dave M. Three-dimensional Euler solutions on blocked grids using an implicit two-pass algorithm. American Institute of Aeronautics and Astronautics, 1987.

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19

Berger, Marsha J. Stable boundary conditions for Cartesian grid calculations. Institute for Computer Applications in Science and Engineering, 1990.

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20

Hawken, D. F. Review of adaptive-grid techniques for solution of partial differential equations. [s.n.], 1987.

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21

Hawken, D. F. Review of adaptive-grid techniques for solution of partial differential equations. Institute for Aerospace Studies, 1985.

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22

Wilkinson, Andrew R. Numerical solution of the Euler equations for transonic airfoil flows using unstructured grids. National Library of Canada = Bibliothèque nationale du Canada, 1992.

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23

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

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24

S, Clark William. Prediction of unsteady flows in turbomachinery using the linearized Euler equations on deforming grids. National Aeronautics and Space Administration, 1991.

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25

S, Clark William. Prediction of unsteady flows in turbomachinery using the linearized Euler equations on deforming grids. National Aeronautics and Space Administration, 1994.

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26

Mavriplis, Dimitri J. Euler and Navier-Stokes computations for two-dimensional geometries using unstructured meshes. Institute for Computer Applications in Science and Engineering, 1990.

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27

Sidilkover, D. Some approaches towards constructing optimally efficient multigrid solvers for the inviscid flow equations. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1997.

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28

Kinard, Tom A. Euler technology assessment for preliminary aircraft design - compressibility predictions by employing the unstructured grid USM3D code. Langley Research Center, 1996.

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29

Finley, Dennis B. Euler technology assessment for preliminary aircraft design - compressibility predictions by employing the Cartesian unstructured grid SPLITFLOW code. Langley Research Center, 1996.

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30

Berger, Martin J. Stable boundary conditions for Cartesian grid calculations. National Aeronautics and Space Administration, Langley Research Center, 1990.

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31

Singh, K. P. 3-D unstructured method for flows past bodies in 6-DOF relative motion: Preprint from proceedings of 6th International Symposium of Computational Fluid Dynamics, Japan Society of Computational Fluid Dynamics, September 4-8, 1995, Lake Tahoe, Nevada. National Aeronautics and Space Administration, 1995.

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32

Frink, Neal T. Tetrahedral finite-volume solutions to the Navier-Stokes equations on complex configurations. National Aeronautics and Space Administration, Langley Research Center, 1998.

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33

Caughey, D. A. Multigrid methods for aerodynamic problems in complex geometries: Final report. National Aeronautics and Space Administration, 1995.

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34

Caughey, D. A. Multigrid calculation of three-dimensional turbomachinery flows. Fluid Dynamics and Aerodynamics Program, Sibley School of Mechanical and Aerospace Engineering, Cornell University, 1989.

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35

United States. National Aeronautics and Space Administration. and Mississippi State University. Dept. of Aerophysics and Aerospace Engineering., eds. Adaptive grid embedding for the two-dimensional flux-split Euler equations. Mississippi State University, Dept. of Aerospace Engineering, 1990.

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36

Zonal multigrid solution of compressible flow problems on unstructured and adaptive meshes. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1989.

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37

Accurate multigrid solution of the Euler equations on unstructured and adaptive meshes. NASA Langley Research Center, 1988.

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38

United States. National Aeronautics and Space Administration., ed. A Cartesian, cell-based approach for adaptively-refined solutions of the Euler and Navier-Stokes equations. National Aeronautics and Space Administration, 1994.

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39

United States. National Aeronautics and Space Administration., ed. A Cartesian, cell-based approach for adaptively-refined solutions of the Euler and Navier-Stokes equations. National Aeronautics and Space Administration, 1994.

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40

United States. National Aeronautics and Space Administration., ed. An adaptively-refined, Cartesian cell-based scheme for the Euler and Navier-Stokes equations. National Aeronautics and Space Administration, 1994.

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41

An adaptively-refined, Cartesian cell-based scheme for the Euler and Navier-Stokes equations. National Aeronautics and Space Administration, 1994.

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42

United States. National Aeronautics and Space Administration., ed. An adaptively-refined, Cartesian cell-based scheme for the Euler and Navier-Stokes equations. National Aeronautics and Space Administration, 1994.

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43

T, Batina John, Williams Marc H, and United States. National Aeronautics and Space Administration., eds. Temporal-adaptive Euler/Navier-Stokes algorithm for unsteady aerodynamic analysis of airfoils using unstructured dynamic meshes. National Aeronautics and Space Administration, 1990.

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44

T, Batina John, Williams Marc H, and United States. National Aeronautics and Space Administration., eds. Temporal-adaptive Euler/Navier-Stokes algorithm for unsteady aerodynamic analysis of airfoils using unstructured dynamic meshes. National Aeronautics and Space Administration, 1990.

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45

T, Batina John, Williams Marc H, and United States. National Aeronautics and Space Administration., eds. Temporal-adaptive Euler/Navier-Stokes algorithm for unsteady aerodynamic analysis of airfoils using unstructured dynamic meshes. National Aeronautics and Space Administration, 1990.

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46

1934-, Jameson Antony, and Langley Research Center, eds. Multigrid solution of the Euler equations on unstructured and adaptive meshes. National Aeronautics and Space Administration, Langley Research Center, 1987.

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47

Holmes, D. G. Solution of the 2D Navier-Stokes equations on unstructur adaptive grids. 1989.

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48

United States. National Aeronautics and Space Administration., ed. Development of an unstructured solution adaptive method for the quasi-three-dimensional Euler and Navier-Stokes equations. National Aeronautics and Space Administration, 1993.

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49

1934-, Jameson Antony, and United States. National Aeronautics and Space Administration, eds. An multigrid LU-SSOR scheme for approximate Newton iteration applied to the Euler equations. National Aeronautics and Space Administration, 1986.

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50

1934-, Jameson Antony, and United States. National Aeronautics and Space Administration, eds. An multigrid LU-SSOR scheme for approximate Newton iteration applied to the Euler equations. National Aeronautics and Space Administration, 1986.

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