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1

Chattot, Jean-Jacques. Computational Aerodynamics and Fluid Dynamics. Berlin, Heidelberg: Springer Berlin Heidelberg, 2002. http://dx.doi.org/10.1007/978-3-662-05064-4.

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2

Tucker, Paul G. Advanced computational fluid and aerodynamics. Cambridge: University of Cambridge, 2016.

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3

Engineers, Society of Automotive, and SAE International Congress & Exposition (1992 : Detroit, Mich.), eds. Vehicle aerodynamics: Wake flows, computational fluid dynamics, and aerodynamic testing. Warrendale, PA: Society of Automotive Engineers, 1992.

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4

1936-, Thornton Earl A., Wieting A. R, and Langley Research Center, eds. Fluid-thermal-structural study of aerodynamically heated leading edges. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.

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5

1936-, Thornton Earl A., Wieting A. R, and Langley Research Center, eds. Fluid-thermal-structural study of aerodynamically heated leading edges. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.

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6

Chattot, Jean-Jacques. Computational Aerodynamics and Fluid Dynamics: An Introduction. Berlin, Heidelberg: Springer Berlin Heidelberg, 2002.

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7

United States. National Aeronautics and Space Administration., ed. Interactive computer graphics applications for compressible aerodynamics. [Washington, DC]: National Aeronautics and Space Administration, 1994.

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8

Center, Ames Research, ed. A Perspective of computational fluid dynamics. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1986.

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9

A, Arndt Roger E., American Society of Civil Engineers. Aerospace Division., American Society of Civil Engineers. Engineering Mechanics Division., and American Society of Civil Engineers. Hydraulics Division., eds. Advancements in aerodynamics, fluid mechanics, and hydraulics: Proceedings of the specialty conference. New York, N.Y: The Society, 1986.

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10

K, Bose T. Computational fluid dynamics. New York: Wiley, 1988.

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11

Jacques, Periaux, European Computational Aerodynamics Research Project., and European Commission. Directorate-General XII, Science, Research, and Development., eds. Optimum aerodynamic design & parallel Navier-Stokes computations: ECARP, European Computational Aerodynamics Research Project. Braunschweig/Wiesbaden: Vieweg, 1998.

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12

1931-, Tanida Y., and Namba M. 1936-, eds. Unsteady aerodynamics and aeroelasticity of turbomachines. Amsterdam: Elsevier, 1995.

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13

Sanford, Fleeter, and United States. National Aeronautics and Space Administration., eds. Aerodynamics of a linear oscillating cascade. [Washington, DC: National Aeronautics and Space Administration, 1990.

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14

Elsner, Janusz W. Aerodynamika palisad łopatkowych. Wrocław: Zakład Narodowy im. Ossolińskich, 1988.

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15

Inouye, Mamoru. A decade of computer simulations for space shuttle aerodynamics. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1988.

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16

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Aerodynamics of 3-D aircraft afterbodies. Neuilly-sur-Seine: AGARD, 1995.

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17

N, Tiwari S., and United States. National Aeronautics and Space Administration., eds. Grid sensitivity for aerodynamic optimization and flow analysis. Norfolk, Va: Old Dominion University Research Foundation, Dept. of Mechanical Engineering and Mechanics, College of Engineering and Technology, Old Dominion University, 1993.

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18

N, Tiwari S., and United States. National Aeronautics and Space Administration., eds. Grid sensitivity for aerodynamic optimization and flow analysis. Norfolk, Va: Old Dominion University Research Foundation, Dept. of Mechanical Engineering and Mechanics, College of Engineering and Technology, Old Dominion University, 1993.

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19

Ballmann, Josel, Richard Eppler, and Wolfgang Hackbusch, eds. Panel Methods in Fluid Mechanics with Emphasis on Aerodynamics. Wiesbaden: Vieweg+Teubner Verlag, 1988. http://dx.doi.org/10.1007/978-3-663-13997-3.

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20

Center, Langley Research, ed. Unstructured-grid methods development, lessons learned. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

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21

Center, Langley Research, ed. Unstructured-grid methods development, lessons learned. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

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22

1948-, Smith F. T., and Langley Research Center, eds. On strongly nonlinear vortex/wave interactions in boundary-layer transition. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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23

O, Seddougui Sharon, and Langley Research Center, eds. A note concerning the onset of three dimensionality and time dependence in Görtler vortices. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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24

Philip, Hall, Zang Thomas A, and Langley Research Center, eds. On the nonlinear interaction of Gortler vortices and Tollmien-Schlichting waves in curved channel flows at finite Reynolds numbers. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.

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25

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

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26

Center, Langley Research, ed. Unstructured-grid methods development, lessons learned. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

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27

Bryan, Thwaites, ed. Incompressible aerodynamics: An account of the theory and observation of the steady flow of incompressible fluid past aerofoils, wings, and other bodies. New York: Dover Publications, 1987.

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28

Center, Langley Research, ed. A nonlinear investigation of the stationary modes of instability of the three-dimensional compressible boundary layer due to a rotating disc. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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29

M, Thomas A., and United States. National Aeronautics and Space Administration., eds. Investigation of radiative interactions in supersonic internal flows: Progress report for the period ended May 31, 1991. Norfolk, Va: Old Dominion University Research Foundation, 1991.

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30

Shigeru, Obayashi, and Ames Research Center, eds. A streamwise upwind algorithm applied to vortical flow over a delta wing. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1990.

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31

L, Streett Craig, Hussaini M. Yousuff, and Langley Research Center, eds. An analysis of artificial viscosity effects on reacting flows using a spectral multi-domain technique. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.

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32

Hall, Philip. On the Goertler vortex instability mechanism at hypersonic speeds. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.

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33

Hoerner, Sighard F. Fluid-dynamic lift: Practical information on aerodynamic and hydrodynamic lift. 2nd ed. [Brick Town, N.J.]: L.A. Hoerner, 1985.

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34

Lee, Elizabeth M. Conical Euler solution for a highly-swept delta wing undergoing wing-rock motion. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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35

N, Gupta Roop, Shinn Judy L, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Conservation equations and physical models for hypersonic air flows in thermal and chemical equilibrium. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

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36

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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37

C, Yee Henry, Kutler Paul, and Ames Research Center, eds. Numerical study of unsteady viscous hypersonic blunt body flows with an impinging shock. Moffet Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1988.

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38

Center, Ames Research, ed. Transonic Navier-Stokes computations of strake-generated vortex interactions for a fighter-like configuration. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1988.

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39

Center, Ames Research, ed. Transonic Navier-Stokes computations of strake-generated vortex interactions for a fighter-like configuration. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1988.

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40

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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41

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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42

Ramm, Heinrich J. Fluid dynamics for the study of transonic flow. New York: Oxford University Press, 1990.

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43

L, Fezoui, Periaux Jacques, and Hunt Julian C. R, eds. Computational aeronautical fluid dynamics. Oxford: Clarendon Press, 1994.

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44

E, Lawson Robert, and United States. Environmental Protection Agency., eds. Fluid modeling simulation of stack-tip downwash for neutrally buoyant plumes. [Washington, D.C.?: U.S. Environmental Protection Agency, 1992.

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45

Wolf-Heinrich, Hucho, ed. Aerodynamics of road vehicles: From fluid mechanics to vehicle engineering. 4th ed. Warrendale, PA: Society of Automotive Engineers, 1998.

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46

Kantha, Lakshmi. Migration on Wings: Aerodynamics and Energetics. Berlin, Heidelberg: Springer Berlin Heidelberg, 2012.

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47

NATO Advanced Study Institute on Molecular Physics and Hypersonic Flows (1995 Maretea, Italy). Molecular physics and hypersonic flows: [proceedings of the NATO NATO Advanced Study Institute on Molecular Physics and Hypersonic Flows, Maretea, Italy, May 21-June 3, 1995]. Dordrecht: Kluwer Academic in cooperation with NATO Scientific Affairs Division, 1996.

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48

United States. Army Aviation Research and Technology Activity. and Ames Research Center, eds. Some rotorcraft applications of computational fluid dynamics. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1988.

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49

Smith, J. H. B. Fluid Dynamics Panel symposium 'Vortex flow aerodynamics' technical evaluation report. London: HMSO, 1991.

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50

S, Liou M., Povinelli Louis A, and United States. National Aeronautics and Space Administration., eds. Navier-Stokes analysis of transonic cascade flow. [Washington, DC]: National Aeronautics and Space Administration, 1990.

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