Computations of high-lift airfoil flows using two-equation turbulence models

37th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1999, Pages

  Kim, Chang Sung ^a,b   Kim, Chongam ^a,b   Rho, Oh Hyun ^a,b  

^a Seoul National University   (South Korea)

^b Dep t of Aerospace Engineering   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; BOUNDARY LAYERS; FLOW MEASUREMENT; FLOW SEPARATION; INCOMPRESSIBLE FLOW; NASA; NAVIER STOKES EQUATIONS; TURBULENCE MODELS;

ADVERSE PRESSURE GRADIENT; COMPRESSIBLE NAVIER-STOKES; DUAL TIME STEPPING METHOD; MULTI ELEMENT AIRFOILS; SURFACE PRESSURE COEFFICIENTS; TWO-EQUATION TURBULENCE MODELS; UPWIND DIFFERENCING SCHEMES; VISCOUS TURBULENT FLOW;

AIRFOILS;

EID: 84983203345     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1999-542     Document Type: Conference Paper

References (16)

1. Brune, G. W. and McMasters, J. H., “Computa-tional Aerodynamics Applied to High-Lift System,” Edited by P. A. Henne, Progress in Astro-nautics and Aeronautics, Vol. 125, 1990, 389-493.
2. Wilcox, D. C, “Reassessment of the Scale-Determining Equation for Advanced Turbulence Models,” AIAA Journal, Vol. 26, No. 11, 1988, 1299-1310.
3. Wiícox, D. C, “Simulation of Transition with a Two-Equation Turbulence Model,” AIAA Joumal, Vol. 32, No. 2, Feb. 1994, 247-255.
4. Menter, F. R., “Influence of Freestream Values on the k-ω Turbulence Model Predictions,” AIAA Journal, Vol. 30, No. 6, August 1992, 16511659.
5. Menter, F. R., “Two-Equation Eddy-Viscosity turbulence Models for Engineering Applications,” AIAA Journal, Vol. 32, No. 8, August 1994, 1598-1605.
6. Roe, P. L., “Approximate Riemann Solvers, Parameter Vectors and Difference Schemes,” Joumal of Computational Physics, Vol.43, 1983, 357-372.
7. Hwang, S. W., “Numerical Analysis of Unsteady Supersonic Flow over Double Cavity,” Ph.D. Dis-sertation, Seoul Nat’l Univ., Seoul, Korea, 1996.
8. Yoon, S. and Kwak, D., “Three-Dimensional In-compressible Navier-Stokes Solver Using Lower-Upper Symmetric-Gauss-Seidel Algorithm,” AIAA Joumal, Vol. 29, June 1991, 874-875.
9. Rogers, S. E. and Kwak, D., “Upwind Differenc-ing Scheme for the Time Accurate Incompressible Navier-Stokes Equations,” AIAA Journal, Vol. 28, No. 2, February 1990, 253-262.
10. Rogers, S. E., Wiltberger, N. L., Kwak, D., “Effi-cient Simulation of Incompressible Viscous Flow over Single and Multielement Airfoils,” Journal ofAircraft, Vol.30, No.5, Sept-Oct. 1993, 736-743.
11. Steger, J. L., Doughty, F. C, and Beneck, J. A., “A Chimera Grid Scheme,” Advances in Grid Gen-eration, FED, Vol.5, ASME, Edited by Ghia, K. N., New York, 1983, 59-69.
12. Cook, P. H., McDonald, M. A. and Firmin, M. C. R, “Aerofoil RAE 2822 - Pressure Distributíons, and Boundary Layer and Wake Measurements,” AGARD AR 138, May 1979, A6-1 to A6-77.
13. Coles, D., and Wadcock, A. J., “Flying-Hot-Wire Study of Flow Pat an NACA 4412 Airfoil at Maximum Lift,” AIAA Journal, Vol. 17, April 1979, 321-329.
14. McGhee, R J, and Beasley, W. D., “Low-speed aerodynmic characteristics of a 17-percent-thick airfoil section designed for general aviation applications,” NASA TN D-7428, N74-11821, 1973.
15. Berg, B. v. d., “Boundary Layer Measurements On a Two-Dimensional Wing With Flap,” NLR TR 79009 U, Jan. 1997.
16. Braden, J. A., Whipkey, R. R., Jones, G. S., and Lilley, D. E., “Experimental Study of the Sepa-rating Confluent Boundary-Layer,” NASA Con-tractor Report 3655.