1 |
2007, Lian, Y., and Shyy, W., "Laminar-Turbulent Transition of a Low Reynolds Number Rigid or Flexible Airfoil," AIAA Journal, Vol.45, No.7, pp.1501-1513.
DOI
ScienceOn
|
2 |
2006, Cliquet, J., and Houderville, R., "New Development in Transition Computation in the elsA Navier-Stokes Solver," 7th ONERA-DLR Aerospace Symposium(ODAS).
|
3 |
2008, Cliquet, J., Houderville, R., and Arnal, D., "Application of Laminar-Turbulent Transition Criteria in Navier-Stokes Computations," AIAA Journal, Vol.46, No.5, pp.1183-1190.
|
4 |
2008, Perraud, J., Cliquet, J., Houdeville, R., and Arnal, D., "Transport Aircraft Three-Dimensional High-Lift-Wing Numerical Transition Prediction," Journal of Aircraft, Vol.45, No.5, pp.1554-1563.
DOI
ScienceOn
|
5 |
2006, Menter, F.R., Langtry, R.B., and Volker, S., "Transition Modeling for General Purpose CFD Codes," Flow Turbulence Combust, Vol.77, pp.277-303.
DOI
|
6 |
2009, Langtry, R.B., and Menter, F.R., "Correlation-Based Transition Modeling for Unstructured Parallelized Computational Fluid Dynamics Codes," AIAA Journal, Vol.47, No.12, pp.2894-2096.
DOI
ScienceOn
|
7 |
2006, Langtry, R.B., "A Correlation-Based Transition Model using Local Variables for Unstructured Parallelized CFD codes," Ph.D. Thesis, Univ. of Stuttgart, Stuttgart, Germany.
|
8 |
2004, Park, S.H., and Kwon, J.H., "Implementation of Turbulence Models in an Implicit Multigrid Method," AIAA Journal, Vol.42, No.7, pp.1348-1357.
DOI
ScienceOn
|
9 |
2001, Drela, M., "XFOIL 6.94 User Guide," MIT Department of Aeronautics and Astronautics.
|
10 |
1953, Granville, P.S., "The Calculation of the Viscous Drag of Bodies of Revolution," AGARD Rep. 849, David W. Taylor Model Basin.
|
11 |
2007, Drela, M., "A User's Guide to MSES 3.05," MIT Department of Aeronautics and Astronautics.
|
12 |
1981, Roe, P.L., "Approximate Riemann Solvers, Parameter Vectors, and Difference Schemes," Journal of Computational Physics, Vol.43, No.2, pp.357-372.
DOI
ScienceOn
|
13 |
1979, van Leer, B., "Towards the Ultimate Conservative Difference Scheme, V. A Second Order Sequel to Godunov's Method," Journal of Computational Physics, 32, pp.101-136.
DOI
ScienceOn
|
14 |
1981, Pulliam, T.H., and Chaussee, D.S., "A Diagonal Form of an Implicit Approximate Factorization Algorithm," Journal of Computational Physics, Vol.39, Feb, pp.347-363.
DOI
ScienceOn
|
15 |
1970, Gregory, N., and O'Reilly, C.L., "Low-Speed Aerodynamic Characteristics of NACA0012 Airfoil Section, Including The Effects of Upper-Surface Roughness Simulation Hoar Frost," Tech. rep., NPL AERO Rept. 1308.
|
16 |
1991, Hicks, R.M., and Cliff, S.E., "An Evaluation of Three Two-Dimensional Computational Fluid Dynamic Codes Including Low Reynolds Numbers and Transonic Mach Numbers," NASA TM-102840, Ames Research Center, California.
|
17 |
1994, von Doenhoff, A.E., and Stivers, L.S., Jr., "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., NACA-CB-L4I25.
|
18 |
1992, Pulliam, T.H., "Solution Methods In Computational Fluid Dynamics," Technical report, NASA Ames Research Center.
|
19 |
1956, van Ingen, J., "A Suggested Semi-Empirical Method for the Calculation of the Boundary-Layer Region," Tech. rep., Delft, Holland, Rept. No.VTH71, VTH74.
|
20 |
1986, Drela, M., and Giles, M.B., "Viscous-Inviscid Analysis of Transonic and Low Reynolds Number Airfoils," AIAA 1987, Vol.25, No.10, pp.1347-1355.
|
21 |
1989, Drela, M., "XFOIL: An Analysis and Design for Low Reynolds Number Airfoils," Low Reynolds Number Aerodynamics, Springer-Verlag.
|
22 |
1991, HerBert, T., "Boundary-Layer Transition-Analysis and Prediction Revisited," AIAA 91-0734.
|
23 |
1991, Bertolotti, F.P., "Linear and Nonlinear Stability of Boundary Layer with Streamwise Varying Properties," Ph.D Thesis, Ohio State University.
|
24 |
1956, Smith, A.M.O., and Gamberoni, N., "Transition, Pressure Gradient and Stability Theory," Douglas Aircraft Co., Report. ES 26 388.
|