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1

Finite element methods for viscous incompressible flows: A guide to theory, practice, and algorithms. Academic Press, 1989.

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2

Shigemi, Masashi. Finite element analysis of incompressible viscous flows around single and multi-element aerofoils in high Reynolds number region. National Aerospace Laboratory, 1988.

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3

Nakahashi, Kazuhiro. FDM-FEM zonal method for viscous flow computations over multiple-bodies. National Aerospace Laboratory, 1987.

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4

T. F. O. de Mulder. FEGAS: A finite element solver for 2D viscous incompressible gas flows using SUPG/PSPG stabilized piecewise linear equal-order velocity-pressure interpolation on unstructured triangular grids. Von Karman Institute for Fluid Dynamics, 1994.

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5

Girault, Vivette. Finite element methods for Navier-Stokes equations: Theoryand algorithms. Springer-Verlag, 1986.

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6

Baker, A. J. Analysis of boundary conditions for SSME subsonic internal viscous flow analysis. Computational Mechanics Corporation, 1986.

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7

Baker, A. J. Analysis of boundary conditions for SSME subsonic internal viscous flow analysis. Computational Mechanics Corporation, 1986.

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8

1939-, Raviart Pierre-Arnaud, and Girault Vivette 1943-, eds. Finite element methods for Navier-Stokes equations: Theory and algorithms. Springer-Verlag, 1986.

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9

Jiang, Bo-Nan. A least-squares finite element method for incompressible Navier-Stokes problems. Lewis Research Center, 1989.

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10

Jiang, Bo-Nan. A least-squares finite element method for incompressible Navier-Stokes problems. Lewis Research Center, 1989.

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11

Jiang, Bo-Nan. A least-squares finite element method for incompressible Navier-Stokes problems. Lewis Research Center, 1989.

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12

Jiang, Bo-Nan. A least-squares finite element method for incompressible Navier-Stokes problems. Lewis Research Center, 1989.

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13

Mulder, T. F. O. De. FEGAS: A finite element solver for 2D viscous incompressible gas flows using SUPG/PSPG stabilized piecewise linear equal-order velocity-pressure interpolation on unstructured triangular grids. von Karman Institute for Fluid Dynamics, 1994.

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14

Lafe, O. A global interpolation function (GIF) boundary element code for viscous flows. American Institute of Aeronautics and Astronautics, 1995.

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15

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

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16

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

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17

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

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18

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

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19

Riedelbauch, Stefan. The simulation of three-dimensional viscous supersonic flow past blunt bodies with a hybrid implicit/explicit finite-difference method. DFVLR, 1987.

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20

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

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21

L, Lin T., Povinelli Louis A, and United States. National Aeronautics and Space Administration., eds. Large-scale computation of incompressible viscous flow by least-squares finite element method. National Aeronautics and Space Administration, 1993.

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22

L, Lin T., Povinelli Louis A, and United States. National Aeronautics and Space Administration., eds. Large-scale computation of incompressible viscous flow by least-squares finite element method. National Aeronautics and Space Administration, 1993.

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23

L, Lin T., Povinelli Louis A, and United States. National Aeronautics and Space Administration., eds. Large-scale computation of incompressible viscous flow by least-squares finite element method. National Aeronautics and Space Administration, 1993.

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24

United States. National Aeronautics and Space Administration., ed. The semi-discrete Galerkin finite element modelling of compressible viscous flow past an airfoil: Final technical report. National Aeronautics and Space Administration, 1992.

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25

United States. National Aeronautics and Space Administration., ed. The semi-discrete Galerkin finite element modelling of compressible viscous flow past an airfoil: Final technical report. National Aeronautics and Space Administration, 1992.

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26

United States. National Aeronautics and Space Administration., ed. The semi-discrete Galerkin finite element modelling of compressible viscous flow past an airfoil: Final technical report. National Aeronautics and Space Administration, 1992.

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27

M, Hafez M., and Kwak Dochan, eds. Numerical simulations of incompressible flows. World Scientific, 2003.

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28

Finite Element Methods for Viscous Incompressible Flows. Elsevier, 1989. http://dx.doi.org/10.1016/c2009-0-22263-x.

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29

Shlomo, Taasan, and Institute for Computer Applications in Science and Engineering, eds. Mathematical aspects of finite element methods for incompressible viscous flows. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1986.

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30

University of Wales. Institute for Numerical Methods in Engineering. and Langley Research Center. Aerothermal Loads Branch., eds. Finite element methods of analysis for high speed viscous flows. Aerothermal Loads Branch, Loads and Aeroelasticity Division, NASA Langley Research Center, 1987.

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31

R, Reddy D., Cheng A. H. -D, and United States. National Aeronautics and Space Administration., eds. A global interpolation function (GIF) boundary element code for viscous flows. American Institute of Aeronautics and Astronautics, 1995.

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32

Rapid numerical simulation of viscous axisymmetric flow fields. National Aeronautics and Space Administration, 1995.

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33

Dimitri, Mavriplis, and Institute for Computer Applications in Science and Engineering., eds. Implicit method for the computation of unsteady flows on unstructured grids. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1995.

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34

Dimitri, Mavriplis, and Institute for Computer Applications in Science and Engineering., eds. Implicit method for the computation of unsteady flows on unstructured grids. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1995.

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35

United States. National Aeronautics and Space Administration., ed. Development of an upwind, finite-volume code with finite-rate chemistry. MCAT Institute, 1995.

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36

United States. National Aeronautics and Space Administration., ed. Development of an upwind, finite-volume code with finite-rate chemistry. MCAT Institute, 1994.

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37

Isaac, Greber, and United States. National Aeronautics and Space Administration., eds. Three dimensional compressible turbulent flow computations for a diffusing S-duct with/without vortex generators. National Aeronautics and Space Administration, 1994.

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38

Center, Langley Research, and United States. National Aeronautics and Space Administration., eds. Euler technology assessment: SPLITFLOW code applications for stability and control analysis on an advanced fighter model employing innovative control concepts. National Aeronautics and Space Administration, Langley Research Center, 1998.

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