Experimental Investigation of Transonic Aerofoil Shock/ Boundary Layer Interaction Control Using Streamwise Slots

Author:

Smith A. N.,Babinsky H.,Fulker J. L.,Ashill P. R.

Publisher

Springer Netherlands

Reference7 articles.

1. Fulker J L AND Simmons M J [1997] An experimental investigation of passive shock / boundary-layer control on an aerofoil, Notes on Numerical Fluid Mechanics, Vol. 56, Euroshock-Drag Reduction by Passive Shock Control, edited by E Stanewsky, J Délery, J Fulker and W Geissler, Vieweg, pp 379–385.

2. Fulker J L AND Simmons M J [1999] An investigation of active, suction, shock and boundary layer control techniques, DERA Technical Report, DERA-/MSS4X/CR980817/1.0.

3. Ashill P R, Fulker J L and Hackett K C [2001] Research at DERA on sub-boundary layer vortex generators, AIAA Paper 2001-0887

4. Lock C N H, Hilton W F and Goldstein S [1940] Determination of profile drag at high speeds by Pitot traverse methods, ARC R&M 1970.

5. Pearcey H H, Haines A B and Osborne J [1968] The interaction between local effects at the shock and rear separation — a source of significant scale effects in wind-tunnel tests on aerofoils and wings, AGARD CP35-11.

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1. Three-Dimensional SBLI Control for Transonic Wings;3rd AIAA Flow Control Conference;2006-06-05

2. A Review of Research at Qinetiq on the Control of Shock Waves;IUTAM Symposium Transsonicum IV;2002

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