Normal shock wave/turbulent boundary-layer interaction control using 'smart' piezoelectric actuators

Aeronautical Journal

Volumn 109, Issue 1101, 2005, Pages 577-583

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

^a UNIVERSITY OF NEW SOUTH WALES   (Australia)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; BOUNDARY LAYERS; MASS TRANSFER; OPTIMAL CONTROL SYSTEMS; OPTIMIZATION; PIEZOELECTRIC MATERIALS; TURBULENCE;

ACTIVE CONTROL; PLENUM CHAMBER; SMART FLAP ACTUATORS;

SHOCK WAVES;

EID: 29144499296     PISSN: 00019240     EISSN: None     Source Type: Journal    
DOI: 10.1017/S0001924000000919     Document Type: Article

References (26)

1. GREEN, J.E. Interactions between shock waves and turbulent boundary layers, Progress in Aero Sci, 1969, 11, pp 253-340.
2. ALVI, A. and SETTLES, G.S. Physical model of the swept shock wave boundary-layer interaction flowfield, AIAA J, 1992, 30, (9). pp 2252-2258.
3. ATKIN, C.J. and SQUIRE, L.C. A study of the interaction of a normal shock wave with a turbulent boundary layer at Mach numbers between 1.30 and 1.55, Eur J Mech B/Fluids, 1992, 11, (1), pp 93-118.
4. SETTLES, G.S. and DOLLING, D.S. Swept Shock-Wave/Boundary Layer Interactions, Progress in Astron and Aeron, 1992, 141 (SEEBASS A.R. (Ed)), pp 505 - 574.
5. INGER, G.R. Application of a shock-turbulent boundary layer interaction theory in transonic flowfield analysis, AIAA Transonic Perspective Symposium, NASA/Ames Research Center. Moffett Field, California, USA. 18-20 February 1981.
6. KUBOTA, H. and STOLLERY, J.L. An experimental study of the interaction between a glancing shock wave and a turbulent boundary layer, J Fluid Mech, 1982, 116, pp 431 -458.
7. GIBSON, T.M., BABINSKY, H. and SQUIRE, L.C. Passive control of shock wave/boundary layer interactions, Aeronaut J, 2000, pp 124-140.
8. BAHI, L., ROSS, J.M. and NAGAMATSU, H.T. Passive shock wave/boundary layer control for transonic airfoil drag reduction, AIAA 21st Aerospace Sciences Meeting, Reno, NV, USA., January 1983.
9. BABINSKY, H. Control of swept shock wave/turbulent boundary-layer interactions, ISSW22, Imperial College, London, UK, July 18-23 1999.
10. NAGAMATSU, H.T., MITTY, T.J. and NYBERG, G.A. Passive shock wave/ boundary layer control of a helicopter rotor airfoil in a contoured transonic wind tunnel, AIAA 25th Aerospace Sciences Meeting, Reno, Nevada, USA, January 1987.
11. 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 23rd Aerospace Sciences Meeting, Reno, Nevada, USA, January 1985.
12. RAGHUNATHAN, S. Effects of porosity strength on passive shock-wave/boundary layer control AIAA J, 1987, 25, (5), pp 757-758.
13. RAGHUNATHAN, S. GRAY, J.L. and COOPER, R.K. Effects of inclination of holes on passive shock wave boundary layer control, AIAA 25th Aerospace Sciences Meeting, Reno, Nevada, USA, January 1987.
14. RAGHUNATHAN, S. and MABEY, D.G. Passive shock-wave/boundary layer control on a wall-mounted model, 1987, AIAA J, 25, (2), pp 275-278.
15. RAGHUNATHAN, S. Passive control of shock-boundary layer interaction, Progress in Aeros Sci, 1988, 25, pp 271-296
16. SAVU, G. and TRIFU, O. Porous airfoils in transonic flow, 1984, AIAA J, 22 (7 - Technical Notes), pp 989-991.
17. COULDRICK, J.S., GAI, S., MILTHORPE, J. and SHANKAR, K. Development of 'smart' flap actuators for swept shock wave boundary layer interaction control. Australian International Aerospace Conference, Canberra, Australia, 2001.
18. COULDRICK, J.S., GAI, S., MILTHORPE, J. and SHANKAR, K. Swept shock wave boundary layer interaction control with 'smart' flap actuators, 40th AIAA Aerospace Sciences Meeting & Exhibit, Reno, USA, January 2002.
19. COULDRICK, J.S., SHANKAR, K., GAI, S. and MILTHORPE, J. Design optimisation of 'smart' flap actuators for swept shock wave boundary layer interaction control, 2nd Advances in Structural Engineering and Mechanics, Pusan, Korea, 21-23 August 2002.
20. COULDRICK, J.S., GAI, S., MILTHORPE, J. and SHANKAR, K. Active control of swept shock wave/turbulent boundary layer interactions, Aeronaut J. 2004, 108, (2), pp 93-102.
21. COULDRICK, J.S., SHANKAR, K., GAI, S. and MILTHORPE, J. Design of 'smart' flap actuators for swept shock wave/turbulent boundary layer interaction control, Struct Eng and Mech: An Inter Journal, 2003, 16, (5), pp 519-532.
22. SEDDON, J. The flow produced by interaction of a turbulent boundary layer with a normal shock wave of strength sufficient to cause separation, No. 3502, HMSO ARC, R&M London, March 1960.
23. WOOD, B., LOTH, E. and GEUBELLE, P. Mesoflaps for aeroelastic transpiration for SBLI control, AIAA 37th Aerospace Sciences Meeting, Reno, Nevada, USA, January 1999.
24. LEE, Y., HAFENRICHTER, E.S., ORPHANIDES, M.J., DUTTON, J.C., GRAFTON, W., WILKINS, L.J., MCILWAIN, S.T. and LOTH, E., Experimental study of normal shock wave/turbulent boundary-layer interaction control using the SMART system, 40th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, USA, 14-17 January 2002.
25. JAIMAN, R.K., LOTH, E. and DUTTON, J.C., Simulations of normal shock-wave/boundary layer interaction control using mesoflaps, 41st AIAA Aerospace Sciences Meeting & Exhibit, Reno, Nevada, USA, 6-9 January 2003.
26. CRAWLEY, E.F. Intelligent structures for aerospace: a technology overview and assessment, AIAA J, 1994, 32, (8), pp 1689-1699.