참고문헌 (13)

1. Kolmogorov, A. N., "The Equations of Turbulent Motion in an Incompressible Fluid," Isv. Acad. Sci. USSR, Phys. 6 1942, pp. 56-58. 

2. Baldwin, B. S., and Barth, T. J., "A One-Equation Turbulence Transport Model for High Reynolds Number Wall-Bounded Flows," AIAA-91-0610, Jan. 1991. 

3. Spalart, P. R., and Allmaras, S. R., "A One-Equation Turbulence Model for Aerodynamic Flows," AIAA-92-0439, Jan. 1992. 

4. Durbin, P. A., and Yang. Z., "A Transport Equation for Eddy Viscosity," Proceedings of the 1992 Summer Program, Center for Turbulent Research, 1992, pp. 293-303. 

5. Edward, J. R., and McRae, D. S., "Nonlinear Relaxation Navier-Stokes Solver for Three-Dimensional, High-Speed Internal Flows," AIAA Journal., Vol. 31, No. 7, 1993, pp. 1222-1228. 

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6. Baldwin, B. S., and Lomax, H., "Thin Layer Approximate and Algebraic Model for Separated Turbulent Flow," AIAA-78-257, Jan. 1978. 

7. Lombard, C. K., and Bardina, J., "Multi-Dimensional Formulation of CSCM - An Upwind Flux Difference Eigenvector Split Method for the Compressible Navier-Stokes Equations," AIAA-83-1895, July 1983. 

8. 홍승규, 이광섭, “Application of Characteristic Boundary Conditions in the Flux-Difference Splitting Framework,” 대한기계 학회 '99년도 유체공학부문 춘계학술강연회 강연집, pp. 141-156, 한양대학교, 1999. 5. 

9. Cook, P. H., McDonald, M. A., and Firmin, M. C. P., "Aerofoil RAE 2822 Pressure Distributions, and Boundary Layer and Wake Measurements," AGARD AR 138, May 1979, A6-1 to A6-77. 

10. Coles, D., and Wadcock, A. J., "Flying-Hot-Wire Study of Flow Past an NACA 4412 Airfoil at Maximum Lift," AIAA Journal, Vol. 17, April 1979, pp. 321-329. 

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11. Perkins, E. W., and Jorgensen, L. H., "Comparison of Experimental and Theoretical Normal-Force Distributions (Including Reynolds Number Effects) on an Ogive-Cylinder Body at Mach Number 1.98," NACA TN-3716, May, 1956. 

12. Schmitt, V., and Charpin, "Pressure Distributions on the ONERA M6 Wing at Transonic Mach Numbers," Experimental Data Base for Computer Program Assessment. Report of the Fluid Dynamics Panel Working Group 04, AGARD AR 138, May 1979. 

13. Wideman, J. K., Brown, J. L., Miles, J. B., and Ozcan, O., "Surface Documentation of a 3-D Supersonic, Shock-Wave/Boundary-Layer Interaction," NASA TM-108824, June 1994.