Transition on a high-lift swept wing in the European project EUROLIFT

Journal of Aircraft

Volumn 41, Issue 5, 2004, Pages 1183-1190

  Perraud, Jean ^a,b   Séraudie, Alain ^a,b   Moens, Frédéric ^a,c  

^a ONERA   (France)

^b Aerodynamics Department   (France)

^c Applied Aerodynamics Department

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; CONTAMINATION; EXTRAPOLATION; LAMINAR FLOW; LIFT; NAVIER STOKES EQUATIONS; NUMERICAL METHODS; REYNOLDS NUMBER; TRANSPORT AIRCRAFT; TURBULENT FLOW;

EUROLIFT; FLAP DEFLECTION; HIGH-LIFT CONDITION; RELAMINARIZATION; SWEPT WING;

WINGS;

EID: 7544232510     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.4297     Document Type: Article

References (22)

1. Thiede, P., "EUROULIFT - Advanced High Lift Aerodynamics for Transport Aircraft," Air and Space Europe, Vol. 3, No. 3/4, 2001, pp. 1-4.
2. Rudnik, R., Eliasson, P., and Perraud, J., "CFD Methods for Transport Aircraft High Lift Systems," Confederation of European Aerospace Associations, CEAS, Paper 30, London, UK, June 2003.
3. Sérandie, A., Perraud, J., and Moens, F., "Transition. Measurement and Analysis on a Swept Wing in High Lift Configuration," International Council for the Aeronautical Sciences, Aerospace Science and Technology, Vol. 7, No. 8, 2003, pp. 569-576.
4. Arnal, D., "Transition Prediction in Transonic Flows," International Union of Theoretical and Applied Mechanics, Transsonicum III Symposium Göttingen, edited by J. Zierep and H. Oertel, Springer-Verlag, Berlin, 1988, pp. 253-262.
5. Casalis, G., and Arnal, D., "Database Method-Development and Validation of the Simplified Method for Pure Cross-Flow Instability at Low Speed," ONERA, ELFIN II Tech. Rept. 145, Toulouse, France, Dec. 1996.
6. Neitzke, K. P., "Using Advanced Measurement Techniques in High Lift Validation Experiments," Confederation of European Aerospace Associations, CEAS, Paper 31, London, UK, June 2003.
7. Pfenninger, W., "Flow Phenomena at the Leading Edge of Swept Wings," Recent Developments In Boundary Layer Research, AGARDograph 97, PL IV, Bruxelles, Belgium, May 1965.
8. Poll, D. I. A., "Some Aspects of the Flow Near a Swept Attachment Line with Particular Reference to Boundary Layer Transition," Cranfield Inst. of Technology, CoA Rept. 7805, Cranfield, England, U.K., Aug. 1978.
9. Beasley, J. A., "Calculation of the Laminar Boundory Layer and Prediction of Transition on a Sheared Wing," Royal Aeronautical Establishment, Rept. 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 IV, edited by T. Cebeci, Springer-Verlag, 1990, pp. 391-402.
11. Rudnik, R., "CFD Assement for High Lift Flows in the European Project EUROLIFT," AIAA Paper 2003-3794, June 2003.
12. Gazaix, M., Jollès, A., and Lazareff, M., "The elsA Object-Oriented Computational Tool for Industrial Applications," Proceedings of the 23rd Conference of the International Council for the Aeronautical Sciences (ICAS), Toronto, Sept. 2002, Paper 2002-1.10.3.
13. Smith, B. R., "The k-k1 Turbulence Model and Wall Layer Model for Compressible Flows," AIAA Paper 90-1483, June 1990.
14. Smith, B. R., "A Near Wall Model for me k-1 Two Equation Turbulence Model," AIAA Paper 94-2386, June 1994.
15. Eliasson, P., "CFD Improvements for High Lift Flows in the European Project EUROLIFT," AIAA Paper 2003-3795, June 2003.
16. Arnal, D., "Boundary Layer Transition: Predictions Based on Linear Theory," Progress in Transition Modeling, AGARD Rept. 793, Brussels, 1993, pp. 1-63.
17. Smith, A. M. O., and Gamberoni, N., "Transition, Pressure Gradient and Stability Theory," Douglas Aircraft Co., Rept. ES 26388, EI Segondo, CA, 1956.
18. Gregory, N., Stuart, J. T., and Walker, W. S., "On me Stability of Three Dimensional Boundary Layer with Application to 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.
19. Gaster, M., "A Note on the Relation Between Temporally Increasing and Spatially Increasing Disturbances in Hydronamic Stability," Journal of Fluid Mechanics, Vol. 14, 1962, pp. 222-224.
20. Schranf, G., Perraud, J., Vitiello, D., and Lam, F., "Comparison of Boundary Layer Transition Predictions Using Flight Test Data," Journal of Aircraft, Vol. 35, No. 6, 1998, pp. 891-897.
21. Laburthe, F., "Problème de Stabilité Linéaire et Prévision de la Transition dans des Configurations Trirdimensionnelles, Incompressibles et Compressibles," Ph.D. Dissertation, ENSAE, Toulouse, France, Dec. 1992.
22. Airian, Ch., "Stabilité Linéaire et Faiblement Non Linéare d'une Couche Limite Laminaire Incompressible par un Système d'Équations Parabolisées (PSE)," Ph.D. Dissertation, ENSAE, Toulouse, France, June 1994.