Transition prediction and impact on a three-dimensional high-lift-wing configuration

Journal of Aircraft

Volumn 45, Issue 5, 2008, Pages 1751-1766

  Moens, Frédéric ^a   Perraud, Jean ^a,f   Krumbein, Andreas ^b   Toulorge, Thomas ^c,g   Iannelli, Pierluigi ^d,h   Eliasson, Peter ^e,i   Hanifi, Ardeshir ^e,i  

^a ONERA   (France)

^b GERMAN AEROSPACE CENTER DLR   (Germany)

^c INSTITUTO NACIONAL DE TÉCNICA AEROESPACIAL   (Spain)

^d ITALIAN AEROSPACE RESEARCH CENTER   (Italy)

^e SWEDISH DEFENCE RESEARCH AGENCY   (Sweden)

^f CNRS UMR5504   (France)

^g UNIVERSITY OF LEUVEN   (Belgium)

^h Applied Aerodynamics Laboratory

ⁱ Systems and Technology

Author keywords

[No Author keywords available]

Indexed keywords

LIFT; NAVIER STOKES EQUATIONS; REYNOLDS NUMBER;

EUROPEAN PROJECT; HIGH LIFTS; LAMINAR TURBULENT TRANSITIONS; MAXIMUM LIFT COEFFICIENT; REYNOLDS-AVERAGED NAVIER STOKES SOLVERS; TRANSITION PREDICTION; TRANSITION PROCESS; WING CONFIGURATIONS;

WINGS;

EID: 54549092552     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.36238     Document Type: Article

References (31)

1. Haines, A. B., Scale Effects on Aircraft and Weapon Aerodynamics, edited by A. D, Young, AGARDograph AG-323, AGARD, Neuillysur-Seine, France, July 1994, pp. 27-66.
2. Lindblad, I., and de Cock, K., "CFD Prediction of Maximum Lift of a 2-D High-Lift Configuration," 17th ATAA Applied Aerodynamics Conference, AIAA Paper 99-3180, Norfolk, VA, June 1999.
3. Moens, F., "Garteur AD-AG25: CFD Prediction of Maximum Lift of a 2-D High-Lift Configuration," KATnet/GARTEUR High-Lift Workshop, edited by J. Fulker, Stockholm, Sweden, Sept. 2002.
4. Moens, F., Perraud, J., Séraudie, A., and Houdeville, R., "Transition Measurement and Prediction on a Generic High-Lift Swept Wing," Proceedings of the Institution of Mechanical Engineers, Part G (Journal of Aerospace Engineering), Vol. 220 June 2006, pp. 589-603. doi:10.1243/09544100JAERO85
5. Toulorge, T., Ponsin, J., Perraud, J., and Moens, F., "Automatic Transition Prediction for RANS Computations Applied to a Generic High-Lift Wing," 45th AIAA Aerospace Sciences Meeting and Exhibits, AIAA Paper 2007-1086, Reno, NV, Jan. 2007.
6. Krumbein, A., "Automatic Transition Prediction and Application to 3-D High-Lift Configurations," 24th AIAA Applied Aerodynamics Conference, San Francisco, AIAA Paper 2006-3164, June 2006.
7. Pfenninger, W., "Flow Phenomena at the Leading Edge of Swept Wing," Recent Developments in Boundary Layer Research, Pt. 4, AGARDograph AG-97, AGARD, Neuilly-sur-Seine, France, May 1965.
8. Poll, D. I. A., "Some Aspects of the Flow Near a Swept Attachment Line with Particular Reference to Boundary Layer Transition," College of Aeronautics TR 7805, Cranfield, England, U.K., Aug. 1978.
9. Beasley, A., "Calculation of the Laminar Boundary Layer and Prediction of Transition on a Sheared Wing," Royal Aeronautical Establishment, TR 3787, Farnborough, England, U.K., Oct. 1973.
10. Arnal, D., and Juillen, J. C., "Leading Edge Contamination and Relaminarization on a Swept Wing at Incidence," Numerical and Physical Aspects of Aerodynamic Flows 4, edited by T. Cebeci, Springer-Verlag, New York, 1990, pp. 391-402.
11. Arnal, D., "Three-Dimensional Boundary Layers: Laminar-Turbulent Transition," Computations of Three-Dimensional Boundary Layers Including Separation, AGARD Rept. 741, AGARD, Neuilly-sur-Seine, France, 1986.
12. Amal, D., "Transition Prediction in Transonic Flow," IUTAM Symposium Transsonicum 3, Springer-Verlag, Berlin, 1989, pp. 253-262.
13. Casalis, G., and Arnal, D., "ELFIN II Subtask 2.3: Data Base Method Development and Validation of the Simplified Method for Pure Crossflow Instability at Low Speed," ONERA TR 145, Toulouse, France, Dec. 1996.
14. Gregory, N., Stuart, J. T., and Walker, W. S., "On the Stability of Three Dimensional Boundary Layer with Application to the Flow due to a Rotating Disc," Philosophical Transactions of the Royal Society of London, Series A: Mathematical and Physical Sciences, Vol. 248, No 943, 1955, pp. 155-199. doi:10.1098/rsta.1955.0013
15. Gaster, M., "A Note on the Relation Between Temporally Increasing and Spatially Increasing Disturbances in Hydrodynamic Stability," Journal of Fluid Mechanics, Vol. 14, 1962, pp. 222-224. doi: doi:10.1017/S0022112062001184
16. Gleyzes, C., Cousteix, J., and Bonnet, J. L., "Theoretical and Experimental Study of Low Reynolds Number Transitional Separation Bubbles," Proceedings of the Conference on Low Reynolds Number Airfoil Aerodynamics, edited by Th. J, Mueller, Univ. of Notre Dame Notre Dame, IN, June 1985, pp. 137-152.
17. Cliquet, J., Houdeville, R., and Arnal, D., "Application of LaminarTurbulent Transition Criteria in Navier-Stokes Computations," 45th AIAA Aerospace Sciences Meeting and Exhibits, Reno, NV, AIAA Paper 2007-515, Jan. 2007.
18. Perraud, J., and Moens, F., "Transport Aircraft 3-D High-Lift Wing Numerical Transition Prediction," 45th AIAA Aerospace Sciences Meeting and Exhibits, Reno, NV, AIAA Paper 2007-264, Jan. 2007.
19. Wilcox, D. C., "Simulation of Transition with a Two-Equadon Turbulence Model," AIM Journal, Vol. 32, No. 2, Feb. 1994, pp. 247-255.
20. N Method for Determining Onset Transition," 35th AIAA Aerospace Sciences and Exhibit, Reno, NV, AIAA Paper 97-0825, Jan. 1997.
21. Langtry, R. B., and Menter, F. R., "Transition Modeling for General CFD Applications in Aeronautics," 43rd AIAA Aerospace Sciences and Exhibit, Reno, NV, AIAA Paper 2005-522, Jan. 2005.
22. Krimmelbein, N., Radespiel, R., and Nebel, C., "Numerical Aspects of Transition Prediction for Three-Dimensional Configurations," 35th AIAA Fluid Dynamics Conference and Exhibit, Toronto, AIAA Paper 2005-4764, June 2005.
23. Arthur, M. T., Dol, H. S., Krumbein, A., Ponsin, J., and Houdeville, R., "Application of Transition Criteria in Navier-Stokes Computations," Group for Aeronautical Research and Technology in Europe TP-138, Jan. 2003.
24. N Transition Prediction," AIAA Journal, Vol. 43, No 6, June 2005, pp 1221-1229. doi:10.2514/1.12487
25. Krumbein, A., "Automatic Transition Prediction and Application to Three-Dimensional Wing Configurations," Journal of Aircraft, Vol. 44, No. 1, Jan.-Feb. 2007, pp. 119-133. doi:10.2514/1.22254
26. Perrud, J., Séraudie, A., and Moens, F., "Transition on a High-Lift Swept Wing in the European Project EUROLIFT," Journal of Aircraft, Vol. 41, No 5, Sept. 2004, pp. 1183-1190. doi:10.2514/1.4297
27. Kaups, K., and Cebeci, T., "Compressible Laminar Boundary Layers with Suction on Swept and Tapered Wings," Journal of Aircraft, Vol. 14, No 7, July 1977, pp. 661-667.
28. Schrauf, G., "A Note on the Calculation of the Effective Sweep Angle and the Attachment Line Reynolds Number," Messerschmitt-Bolkow-Blohm TR TE 2-1636, Bremen, Germany, 1988.
29. Perraud, J., "Transition Prediction for High Lift Applications, Implementation of Database Method in Boundary Layer Codes and Preliminary Validation," ONERA EUROLIFT TR 2.3-1, Toulouse, France, Jan. 2001.
30. Krumbein, A., Stock, H. W., "Laminar-Turbulent Transition Modeling in Navier-Stokes Solvers Using Engineering Methods," European Congress on Computational Methods in Applied Sciences and Engineering (ECCOMAS 2000) [CD-ROM], International Center for Numerical Methods in Engineering, Barcelona, Sept. 2000.
31. Rudnik, R., and Germain, E., "Re-No Scaling Effects on the EUROLIFT High-Lift Configurations," 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, AIAA Paper 2007-752, Jan. 2007.