Investigation into scale effects on the performance of sub boundary-layer vortex generators on civil aircraft high-lift devices

1st Flow Control Conference

Volumn , Issue , 2002, Pages

  Rae, A J ^a   Galpin, S A ^b   Fulker, J ^a  

^a DEFENCE SCIENCE AND TECHNOLOGY LABORATORY   (United Kingdom)

^b AIRBUS OPERATIONS LTD   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

ADVERSE PRESSURE GRADIENT; AERODYNAMIC PARAMETERS; ATMOSPHERIC WIND TUNNEL; DEPLOYMENT MECHANISMS; FLOW CONTROL DEVICES; HIGH REYNOLDS NUMBER; LOW REYNOLDS NUMBER; LOW-SPEED WIND TUNNEL;

BOUNDARY LAYER FLOW; BOUNDARY LAYERS; FLOW CONTROL; FLOW SEPARATION; REYNOLDS NUMBER; TRANSPORT AIRCRAFT;

WIND TUNNELS;

EID: 84896883372     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (10)

1. D S Woodward and D E Lean, "Where is highlift today? - A review of past UK research programmes", AGARD-CP-515 pp1-1 to 1-45, September 1993.
2. Lin, J. C., "Control of turbulent boundary-layer separation using micro-vortex generators", AIAA 99-3404. 1999.
3. Ashill, P. R., Riddle, G. L. and Stanley, M. J.: Separation control on highly-swept wings with fixed or variable camber, The Aeronautical Journal, October 1995, pp 317-327.
4. C J Betts, P R Ashill and KC Hackett, "Fundamental investigations of the flow downstream of sub boundary-layer control devices". Unpublished.
5. P R Ashill, J L Fulker and K C Hackett, "Studies of flows induced by Sub Boundary-layer Vortex Generators (SBVGs)". Unpublished.
6. P R Ashill, J L Fulker and K C Hackett, "Research at DERA on Sub Boundary-layer Vortex Generators (SBVGs)", AIAA 2001-0887, Reno, January 2001.
7. M Simmons and I J Woodcock, "Tests to evaluate the use of sub-miniature vortex generators on a slotted flap system". Unpublished.
8. S A Galpin, "Vortex generators for high-lift flow control: results from DERA 13x9ft tunnel test". Unpublished.
9. A J Rae and A H Jelly, "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. Unpublished.
10. A J Rae and A H Jelly, "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. Unpublished.