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3 Perraud, J., "Transport Aircraft Three-Dimensional High-Lift-Wing Numerical Transition Prediction" 45 (45): 1554-1563, 2008
4 Smith, A.M.O., "Transition, Pressure Gradient and Stability Theory" 1956
5 Menter, F.R, "Transition Modeling for General Purpose CFD Codes" 77 : 277-303, 2006
6 van Leer, B., "Towards the Ultimate Conservative Difference Scheme, V. A Second Order Sequel to Godunov's Method" 32 : 101-136, 1979
7 Granville, P.S., "The Calculation of the Viscous Drag of Bodies of Revolution" AGARD 1953
8 Pulliam, T.H., "Solution Methods In Computational Fluid Dynamics" NASA Ames Research Center 1992
9 Cliquet, J., "New Development in Transition Computation in the elsA Navier-Stokes Solver" ODAS 2006
10 Gregory, N., "Low-Speed Aerodynamic Characteristics of NACA0012 Airfoil Section, Including The Effects of Upper-Surface Roughness Simulation Hoar Frost" 1970
1 Drela, M, "XFOIL 6.94 User Guide"
2 Drela, M., "Viscous-Inviscid Analysis of Transonic and Low Reynolds Number Airfoils" 25 (25): 1347-1355, 1986
3 Perraud, J., "Transport Aircraft Three-Dimensional High-Lift-Wing Numerical Transition Prediction" 45 (45): 1554-1563, 2008
4 Smith, A.M.O., "Transition, Pressure Gradient and Stability Theory" 1956
5 Menter, F.R, "Transition Modeling for General Purpose CFD Codes" 77 : 277-303, 2006
6 van Leer, B., "Towards the Ultimate Conservative Difference Scheme, V. A Second Order Sequel to Godunov's Method" 32 : 101-136, 1979
7 Granville, P.S., "The Calculation of the Viscous Drag of Bodies of Revolution" AGARD 1953
8 Pulliam, T.H., "Solution Methods In Computational Fluid Dynamics" NASA Ames Research Center 1992
9 Cliquet, J., "New Development in Transition Computation in the elsA Navier-Stokes Solver" ODAS 2006
10 Gregory, N., "Low-Speed Aerodynamic Characteristics of NACA0012 Airfoil Section, Including The Effects of Upper-Surface Roughness Simulation Hoar Frost" 1970
11 Drela, M., "Low Reynolds Number Aerodynamics" Springer-Verlag 1989
12 Bertolotti, F.P., "Linear and Nonlinear Stability of Boundary Layer with Streamwise Varying Properties" Ohio State University 1991
13 Lian, Y., "Laminar-Turbulent Transition of a Low Reynolds Number Rigid or Flexible Airfoil" 45 (45): 1501-1513, 2007
14 Park, S.H., "Implementation of κ-ω Turbulence Models in an Implicit Multigrid Method" 42 (42): 1348-1357, 2004
15 Langtry, R.B., "Correlation-Based Transition Modeling for Unstructured Parallelized Computational Fluid Dynamics Codes" 47 (47): 2894-2096, 2009
16 HerBert, T, "Boundary-Layer Transition-Analysis and Prediction Revisited" AIAA 1991
17 Roe, P.L., "Approximate Riemann Solvers, Parameter Vectors, and Difference Schemes" 43 (43): 357-372, 1981
18 Cliquet, J., "Application of Laminar-Turbulent Transition Criteria in Navier-Stokes Computations" 46 (46): 1183-1190, 2008
19 Hicks, R.M., "An Evaluation of Three Two-Dimensional Computational Fluid Dynamic Codes Including Low Reynolds Numbers and Transonic Mach Numbers" Ames Research Center 1991
20 von Doenhoff, A.E., "Aerodynamic Characteristics of the NACA 747A315 and 747A415 Airfoils from tests in the NACA two-dimensional Low-Turbulence Pressure Tunnel" National Advisory Committee for Aeronautics. Langley Aeronautical Lab 1994
21 Drela, M., "A User’s Guide to MSES 3.05"
22 van Ingen, J., "A Suggested Semi-Empirical Method for the Calculation of the Boundary-Layer Region" 1956
23 Pulliam, T.H., "A Diagonal Form of an Implicit Approximate Factorization Algorithm" 39 : 347-363, 1981
24 Langtry, R.B, "A Correlation-Based Transition Model using Local Variables for Unstructured Parallelized CFD codes" Univ. of Stuttgart 2006