CFD validation for high-lift devices: Two-element airfoil

Transactions of the Japan Society for Aeronautical and Space Sciences

Volumn 49, Issue 163, 2006, Pages 31-39

  Lei, Zhong ^a   Murayama, Mitsuhiro ^a   Takenaka, Keizo ^b   Yamamoto, Kazuomi ^a  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^b MITSUBISHI HEAVY INDUSTRIES LTD   (Japan)

Author keywords

High lift; RANS; Turbulence model; Two dimensional

Indexed keywords

AERODYNAMICS; AIRFOILS; COMPUTATIONAL FLUID DYNAMICS; TURBULENCE; WIND TUNNELS;

HIGH-LIFT; RANS; TURBULENCE MODELS; TWO-DIMENSIONAL;

LIFT;

EID: 33845710533     PISSN: 05493811     EISSN: 05493811     Source Type: Journal    
DOI: 10.2322/tjsass.49.31     Document Type: Article

References (17)

1. Rumsey, C. L. and Ying, S. X.: Prediction of High Lift: Review of Present CFD Capability, Prog. Aerosp. Sci., 38 (2002), pp. 145-180.
2. Murayama, M., Lei, Z., Mukai, J. and Yamamoto, K.: CFD Validation for High-Lift Devices: Three-Element Airfoil, Trans. Jpn. Soc. Aeronaut. Space Sci., 49 (2006), pp. 40-48.
3. Kusunose, K. and Cao, H.: Prediction of Transition Location for a 2-d Navier-Stokes Solver for Multi-Element Airfoil Configurations, AIAA Paper 94-2376, 1994.
4. Krumbein, A.: Automatic Transition Prediction and Application to High Lift Multi-Element Configurations, AIAA Paper 2004-2543, 2004.
5. Van den Berg, B.: Boundary Layer Measurements on a Two-Dimensional Wing with Flap, NLR TR 79009 U, 1979.
6. Haase, W., Chaput, E., Elsholz, E., Leschziner, M. A. and Muller, U. R.: ECARP - European Computational Aerodynamics Research Project: Validation of CFD Codes and Assessment of Turbulence Models, Notes Numer. Fluid Mech., 58 (1997).
7. Takaki, R., Yamamoto, K., Yamane, T., Enomoto, S. and Mukai, J.: The Development of the UPACS CFD Environment, High Performance Computing, Proc. of ISHPC 2003, Springer, Tokyo, 2003, pp. 307-319.
8. http://www.ista.jaxa.jp/aet/cfd/cfd-e01.html
9. Lei, Z.: Effect of RANS Turbulence Models on Computation of Vortical Flows over Wing-Body Configuration, Trans. Jpn. Soc. Aeronaut. Space Sci., 48 (2005), pp. 150-160.
10. Nakahashi, K., Togashi, F., Fujita, T. and Ito, Y.: Numerical Simulations on Separation of Scaled Supersonic Experimental Airplane from Rocket Booster at Supersonic Speed, AIAA Paper 2002-2843, 2002.
11. ) Takenaka, K. and Yamamoto, K.: CFD Analysis and Validation Study of the 2-D High Lift Devices, Proceedings of Aerospace Numerical Simulation Symposium, JAXA SP-04-002, 2004.
12. Spalart, P. R. and Allmaras, S. R.: A One-Equation Turbulence Model for Aerodynamic Flows, AIAA Paper 92-0439, 1992.
13. Spalart, P. R. and Shur, M. L.: On the Sensitization of Turbulence Models to Rotation and Curvature, Aerospace Sci. Technol., 1 (1997), pp. 297-302.
14. Menter, F. R.: Zonal Two Equation k-ω Turbulence Models for Aerodynamic Flows, AIAA Paper 93-2906, 1993.
15. Abid, R.: Evalutions of Tow-Equation Turbulence Models for Prediction of Transitional Flow, Int. J. Eng. Sci., 31 (1993), pp. 831-840.
16. Thomas, J. L. and Salas, M. D.: Far-Field Boundary Conditions for Transonic Lifting Solutions to the Euler Equations, AIAA J., 24 (1986), pp. 1074-1080.
17. Roache, P. J.: Perspective: A Method for Uniform Reporting of Grid Refinement Studies, ASME J. Fluids Eng., 116 (1994), pp. 405-413.