Swept shock wave / turbulent boundary layer interaction control with "smart" flap actuators

40th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2002, Pages

  Couldrick, J ^a   Gai, S ^a   Milthorpe, J ^a   Shankar, K ^a  

^a UNIVERSITY OF NEW SOUTH WALES   (Australia)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; LAMINATED COMPOSITES; MASS TRANSFER; PIEZOELECTRIC ACTUATORS; SHOCK WAVES; SUBSTRATES;

ACTIVE CONTROL; BOUNDARY LAYER INTERACTION; COMPOSITE MATERIAL MECHANICS; FINITE ELEMENT MODELLING; FLAP ACTUATORS; OPTIMUM CONTROL; PLENUM CHAMBER; SMART FLAP ACTUATORS;

BOUNDARY LAYERS;

EID: 85088184499     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-973     Document Type: Conference Paper

References (7)

1. Settles, G.S., and Dolling, D.S., " Swept Shock-Wave/Boundary Layer Interactions", Progress in Astronautics and Aeronautics Vol. 141, Ed-A.R. Seebass, 1992, pp. 505-574.
2. Kubota, H., and Stollery, J.L., "Am Experimental Study of the Interaction Between a Glancing Shock Wave and a Turbulent Boundary Layer, " Journal of Fluid Mechanics, Vol. 116, March 1982, pp. 431-458.
3. Alvi, A., and Settles, G.S., "Physical Model of the Swept Shock Wave Boundary-Layer Interaction Flow field, " AIAA Journal, Vol.30, No.9, 1992, pp. 2252-2258.
4. Babinsky, H., "Control of Swept Shock Wave / Turbulent Boundary-Layer Interactions, " Issw22, London, 18-23 July 1999.
5. Squire, L.C., "Interaction of Swept and Unswept Normal shock Waves with Boundary Layers, " AIAA Journal, Vol. 34, October 1996, pp. 2099-2101.
6. Nagamatsu, H.T., Ficarra, R.V., and Dyer, R., " Supercritical Airofoil Drag Reduction by Passive Shock Wave/Boundary Layer Control in the Mach Number Range.75 to.90, " AIAA Paper 85-0207, 1985.
7. Chen, C., Chow, C, Hoist, T., and Van Dalsem, W., "numerical Study of Porous Airfoils in Transonic Flow, " AIAA Journal, Vol. 22, July 1984, pp. 989-99.