High reynolds-number windtunnel testing for the design of airbus high-lift wings

Notes on Numerical Fluid Mechanics and Multidisciplinary Design

Volumn 92, Issue , 2006, Pages

  Reckzeh, Daniel ^a,b   Hansen, Heinz ^a,b  

^a AIRBUS OPERATIONS GMBH   (Germany)

^b High lift Devices Group   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 84872813186     PISSN: 16122909     EISSN: None     Source Type: Book Series    
DOI: 10.1007/978-3-540-33287-9_1     Document Type: Article

References (16)

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3. Termes P., et al. ; Reynolds and Mach Number effects and the 2D-3D correlation based on measurements and computed results for the Garteur take-off configuration; CEAS Forum on High-Lift and Separation Control, University of Bath (UK), March 1995
4. Fiddes, S.P., Kirby, D.A., Woodward, D.S., Peckham, D.H.; Investigations into the Effects of Scale and Compressibility on Lift and Drag in the RAE 5m Pressurised Low-Speed Wind Tunnel; Aeronautical Journal, Vol. 89, March 1985
5. Lindblad, I.A.A., de Cock, K.M.J.; CFD prediction of Maximum Lift of a 2D High Lift Configuration; AlAA-99-3180;
6. Becker, K., Kroll, N., Rossow, C.C., Thiele, F; MEGAFLOW - A numerical Flow Simulation System; ICAS Paper 98-2.7.4, ICAS Congress 1998; Melbourne, September 1998
7. Arnal, D., Casalis, G., Reneaux, J., Cousteix, J. ; Laminar-Turbulent Transition in Subsonic Boundary Layers : Research and Applications in France; AIAA Paper 97-1905
8. Delery, J.M., Separation in Two and Three-Dimensional Flows: Still a Subject of Mystery ?; VKI, The Jean J. Ginoux Lecture, 1998
9. Thiede, P.; EUROLIFT - Advanced High Lift Aerodynamics for Transport Aircraft; AIR&SPACE EUROPE, Vol. 3 No 3+4, 2001
10. Dargel, G., Schnieder, H.; GARTEUR High Lift Action Group (AG 08) Final Report; GARTEUR TP 043, Nov. 1989
11. Thibert, J.J.; The Garteur High Lift Research Programme; High-Lift System Aerodynamics, CP-515, AGARD, Sept.1993
12. Hansen, H.; Überblick über das Technologieprogramm Hochauftriebskonzepte (HAK); DGLR Jahrestagung, Bremen 1998
13. Quest, J.; ETW - High Quality Test Performance in cryogenic environment; AIAA-00-2206
14. Wright, M.C.N.; Development of the Half Model Testing; Capability at ETW; ICAS 2000
15. Quest, J.; Hansen, H.; Mesura, G.G.; First Measurements on an Airbus High Lift; Configuration at ETW up to Flight Reynolds Number; A1AA-2002-0423
16. Reckzeh, D; Aerodynamc Design of the High-Lift Wing for a Megaliner Aircraft; Aerospace Science & Technology; Oct 2002