Wind tunnel experiments and navier-stokes computations of a high-lift military airfoil

37th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1999, Pages

  Dodbele, S S ^a   Hobbs, C R ^b   Kern, S B ^a   Ghee, T A ^a   Hall, D R ^a   Ely, W L ^b  

^a NAVAL AIR SYSTEMS COMMAND   (United States)

^b NONE   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; AIRFOILS; ANGLE OF ATTACK; COMPUTATIONAL FLUID DYNAMICS; DRAG; FLIGHT CONTROL SYSTEMS; FLOW CONTROL; NASA; NAVIER STOKES EQUATIONS; REYNOLDS NUMBER; SHEAR FLOW; SHEAR STRESS; TURBULENCE MODELS; VORTEX FLOW; WALL FLOW;

FLIGHT REYNOLDS NUMBERS; MICRO VORTEX GENERATORS; MULTI ELEMENT AIRFOILS; NASA LANGLEY RESEARCH CENTER; NAVIER-STOKES COMPUTATIONS; REYNOLDS NUMBER EFFECT; SHEAR-STRESS TRANSPORT; TWO-EQUATION TURBULENCE MODELS;

WIND TUNNELS;

EID: 84983134893     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1999-540     Document Type: Conference Paper

References (11)

1. Meredith, P. T., “Viscous Phenomena Affecting High-Lift Systems and Suggestions for Future CFD Development,” AGARD-CP-515, September 1993, 19-1, 19-8.
2. Hobbs, CR, Spaid, F., Ely, W., and Goodman, W., “High Lift Research Program for a Fighter-type,Multi-Element Airfoil at High Reynolds Numbers,” AIAA 96-0410, January 1996.
3. Baldwin, B. S., and Barth T. J., “A One-Equation Turbulence Transport Model for High Reynolds Number Wall Bounded Flows,” NASA TM 102847, August 1990.
4. Spalart, RR. and Allmaras, S.R., “A One-Equation Turbulence Model for Aerodynamic Flows,” AIAA 92-0439, January 1992.
5. Menter, F.R., “Zonal Two Equation k-w Turbulence Models for Aerodynamic Flows,” AIAA 93-2906, July 1993.
6. Kem, S. B., “Evaluation of Turbulence Models for High-Lift Military Airfoil Flowfields”, AIAA-96-0057, January 1996.
7. Hall, D., and Kern, S., “ Prediction of Reynolds number Effects of Military High-Lift Airfoil”, AIAA 96-2400, June 1996.
8. Cao, H.V., Kusunose, K., Spalart, P.R., Ishimitsu, K.K., Rogers, S.E., and McGhee, R.J., “Study of Wind Tunnel Wall Interference for Multi-Element Airfoils Using a Navier-Stokes Code,” AIAA 941933, June 1994.
9. Rogers, S.E., and Kwak, D., “An Upwind Differ-encing Scheme for the Incompussible Navier-Stokes Equations,” NASA TM 101051, November 1988, also appeared in Applied Numerical Mathematics, Vol. 8, 1991, 43-65.
10. Rogers, S.E., “A Comparison of Implicit Schemes for the Incompressible Navier-Stokes Equations with Artificial Compressibility,” AIAA 95-0567, January 1995.
11. Rogers, S.E., Menter, F.R., Durbin, RA. and Man-sour, N.N., “ A comparison of Turbulence Models in Computing Multi-Element Airfoil Flows,” AIAA 940291, January 1994.