Passive flow control on civil aircraft flaps using sub-boundary layer vortex generators in the AWIATOR programme

Collection of Technical Papers - 3rd AIAA Flow Control Conference

Volumn 1, Issue , 2006, Pages 257-266

  Bohannon, Keith S ^a,b  

^a AIRBUS OPERATIONS LTD   (United Kingdom)

^b AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT LANDING; CIVIL AVIATION; OPTIMIZATION; VORTEX FLOW;

AIRCRAFT FLAPS; PASSIVE FLOW CONTROL; SUB BOUNDARY LAYER VORTEX GENERATORS (SBVG); VORTEX GENERATORS;

FLOW CONTROL;

EID: 33845270733     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2006-2858     Document Type: Conference Paper

References (6)

1. Rae, A. J. and Jelly, A. H., "Test on the application of flow control to the swept/tapered half-model, M477, in the QinetiQ 5 Metre Wind Tunnel during July 2001", QinetiQ 5 Metre Wind Tunnel External Data Report No. 108, QINETIQ/FST/CAT/ CRO12576, February 2002.
2. Galpin, S. A., "Vortex generators for high-lift flow control: results from DERA 13×9ft tunnel test", Airbus UK Technical Note V37/R&T/001821 Issue 1, October 2000.
3. Rae, A. J. and Jelly, A. H., "Test on the application of flow control to the Airbus A380 half-model, X08, in the QinetiQ 5 Metre Wind Tunnel during October 2001", QinetiQ 5 Metre Wind Tunnel External Data Report No. 110, QINETIQ/FST/ CAT/CR021342, February 2002.
4. Galpin, S. A., Rae, A. J. and Fulker, J., "Investigation into Scale Effects on the Performance of Sub Boundary-layer Vortex Generators on Civil Aircraft High-lift Devices", 1st Flow Control Conference, St. Louis, Missouri, June 24-26, 2002.
5. Brunet, V., Francois, C. and Caruana, D., "Vortex Generator Simulations on Transonic and High-Lift Configurations" Paper 16, CEAS/KATnet Conference, Bremen, 20-22 June 2006.
6. Newbold, C. M., "Estimations of boundary layer thickness on the trailing edge flap of the A340-300", QinetiQ Technical Note QinetiQ/FST/TN041582 Issue 1.0, May, 2004.