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

21st AIAA Applied Aerodynamics Conference

Volumn , Issue , 2003, Pages

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

^a ONERA   (France)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; COMPUTATION THEORY; SWEPT WINGS; WIND TUNNELS;

3D CONFIGURATIONS; ATTACHMENT LINES; EUROPEAN PROJECT; EUROPEAN RESEARCH PROJECT; GLOBAL FORCES; LAMINAR-TURBULENT TRANSITION; STABILITY THEORIES; TRANSITION PHENOMENON;

LIFT;

EID: 85067320656     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2003-3796     Document Type: Conference Paper

References (13)

1. P. Thiede, 'EUROLIFT - Advanced High Lift Aerodynamics for Transport Aircraft', AIR & SPACE EUROPE, Vol. 3, No. 3/4, pp. 1-4, 2001
2. R. Rudnik, P. Eliasson, J. Perraud,'CFD Methods for transport aircraft High Lift systems', CEAS Aerospace Aerodynamics Research Conference, London, June 2003
3. A. Séraudie, J. Perraud, F. Moens,"Transition measurement and analysis on a swept wing in high lift configuration", 23rd ICAS, Toronto, Canada, Sept. 2002
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5. G. Casalis, D. Arnal, 'Database method - Development and validation of the simplified method for pure cross-flow instability at low speed', ELFIN II Tech. Rep. No 145, 1996
6. K. P. Neitzke, 'Using Advanced Measurement techniques in High Lift Validation Experiments' CEAS Aerospace Aerodynamics Research Conference, London, June 2003
7. Pfenninger, W., "Flow phenomena at the leading edge of swept wings", Recent developments In Boundary Layer Research, AGARDograph 97, 1965
8. D. I. A. Poll, 'Some aspects of the flow near a swept attachment line with particular reference to boundary layer transition.', Cranfield Institute of Technology, CoA Report No 7805 (1978)
9. J.A. Beasley, 'Calculation of the laminar boundary layer and prediction of transition on a sheared wing' RAE Farnborough Rep. No 3787, 1976.
10. D. Arnal, J. C. Juillen, 'Leading edge contamination and relaminarisation on a swept wing at incidence', Fourth Symp. on Num. and Physical aspects of aerodynamics flows, Calif. State Univ, 1989
11. R. Rudnik, 'CFD Assessment for 3D High Lift Flows in the European Project EUROLIFT', AIAA 2003-3794, Orlando Fl., June 2003
12. P. Eliasson, 'CFD improvements for High Lift Flows in the European Project EUROLIFT', AIAA 2003-3795, Orlando Fl., June 2003
13. G. Schrauf, J. Perraud, D. Vitiello, F. Lam, Comparison of Boundary Layer Transition Predictions using Flight Test Data, Journal of Aircraft, Vol. 35, no 6, 1998