Shock-wave/boundary-layer interaction control using streamwise slots in transonic flows

Journal of Aircraft

Volumn 41, Issue 3, 2004, Pages 540-546

  Smith, A N ^a,d   Babinsky, H ^a,d   Fulker, J L ^b,e   Ashill, P R ^c  

^a UNIVERSITY OF CAMBRIDGE   (United Kingdom)

^b QINETIQ   (United Kingdom)

^c CRANFIELD UNIVERSITY   (United Kingdom)

^d Department of Engineering ^*  (United Kingdom)

^e NATIONAL RESEARCH COUNCIL CANADA   (Canada)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; AIRFOILS; BOUNDARY LAYERS; CONTROL EQUIPMENT; FLOW VISUALIZATION; PRESSURE CONTROL; STREAM FLOW; SUPERSONIC AERODYNAMICS; TRANSONIC FLOW; TURBULENT FLOW; VELOCITY MEASUREMENT; VISCOSITY;

CONTROL DEVICES; STREAMWISE SLOTS; TRANSONIC WINGS; TWO-DIMENSIONAL TRANSONIC AEROFOIL;

SHOCK WAVES;

EID: 3042718258     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.11479     Document Type: Article

References (23)

1. Rosemann, H., Knauer, A., and Stanewsky, E., "Experimental Investigation of the Transonic Airfoils DA LVA1-1A and VA-2 with Shock Control," Notes on Numerical Fluid Mechanics, Euroshock - Drag Reduction by Passive Shock Control, Vol. 56, edited by E. Stanewsky, J. Delery, J. Fulker, and W. Geissler, Vieweg, Brunswick, Germany, 1997, pp. 355-378.
2. Fulker, J. L., and Simmons, M. J., "An Experimental Investigation of Passive Shock/Boundary Layer Control on an Aerofoil," Notes on Numerical Fluid Mechanics, Euroshock - Drag Reduction by Passive Shock Control, Vol. 56, edited by E. Stanewsky, J. Delery, J. Fulker, and W. Geissler, Vieweg, Brunswick, Germany, 1997, pp. 379-386.
3. Raghunathan, S., "Passive Control of Shock-Boundary Layer Interaction," Progress in Aerospace Sciences, Vol. 25, No. 3, 1988, pp. 271-296.
4. Delery, J. M., "Shock Phenomena in High Speed Aerodynamics: Still a Source of Major Concern," The Aeronautical Journal, Vol. 103, No. 1, 1999, pp. 19-34.
5. Bohning, R., and Doerffer, P., "Hybrid and Active Control of the Shock Wave - Turbulent Boundary Layer Interaction and Porous Plate Transpiration Flow," Karlsruhe Univ. Euroshock II Final Technical Rept., Springer Verlag, New York, July 1999.
6. Fulker, J. L., and Simmons, M. J., "An Investigation of Active, Suction, Shock and Boundary Layer Control Techniques," Euroshock II TR CT95-0095/3.1, Springer Verlag, New York, Jan. 1999.
7. Delery, J. M., "Shock Wave/Turbulent Boundary Layer Interaction and its Control," Progress in Aerospace Sciences, Vol. 22, No. 4, 1985, pp. 209-280.
8. Morris, M. J., Sajben, M., and Kroutil, J. C., "Experimental Investigation of Normal-Shock/Turbulent Boundary Layer Interactions with and Without Mass Removal," AIAA Journal, Vol. 30, No. 2, 1992, pp. 359-366.
9. Thiede, P., and Dargel, G., "Assessment of Shock and Boundary Layer Control Concepts for Hybrid Laminar Flow Wing Design," Euroshock II TR BRPR-95-0076, Springer Verlag, New York, Sept. 1999.
10. Ashill, P. R., and Fulker, J. L., "A Review of Flow Control Research at DERA," Proceeding of IUTAM Symposium on Mechanics of Passive and Active Flow Control, edited by G. E. A. Meier and P. R. Viswanath, Kluwer Academic, Norwell, MA, 1999, pp. 43-56.
11. Qin, N., Zhu, Y., Ashill, P. R., and Shaw, S. T., "Active Control of Transonic Aerodynamics Using Suction, Blowing, Bumps and Synthetic Jets," AIAA Paper 2000-4329, Aug. 2000.
12. Lee, B. H. K., "Self-Sustained Shock Oscillations on Airfoils at Transonic Speeds," Progress in Aerospace Sciences, Vol. 37, No. 2, 2001, pp. 147-196.
13. Mabey, D. G., "Unsteady Aerodynamics: Retrospect and Prospect," Aeronautical Journal, Vol. 103, No. 1, 1999, pp. 1-18.
14. de Nicola, C., "Introduction of Passive Shock Control in an Interactive Boundary Layer Method," Notes on Numerical Fluid Mechanics, Euroshock-Drag Reduction by Passive Shock Control, Vol. 56, edited by E. Stanewsky, J. Delery, J. Fulker, and W. Geissler, Vieweg, Brunswick, Germany, 1997, pp. 171-194.
15. Ashill, P. R., Fulker, J. L., and Hackett, K. C., "Research at DERA on Sub Boundary Layer Vortex Generators (SBVGS)," AIAA Paper 2001-0887, Jan. 2001.
16. Pearcey, H. H., "Shock Induced Separation and its Prevention," Boundary Layer and Flow Control, edited by G. V. Lachmann, Pergamon, 1961, pp. 1170-1355.
17. 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 1.3 and 1.55," European Journal of Mechanics B/Fluids, Vol. 11, No. 1, 1992, pp. 93-118.
18. Sun, C., and Childs, M. E., "A Modified Wall Wake Velocity Profile for Turbulent Compressible Boundary Layers," Journal of Aircraft, Vol. 10, No. 6, 1970, pp. 381-383.
19. Coles, D., "The Law of the Wake in the Turbulent Boundary Layer," Journal of Fluid Mechanics, Vol. 1, Pt. 2, 1956, pp. 191-226.
20. Gibson, T. M., Babinsky, H., and Squire, L. C., "Passive Control of Shock Wave Boundary Layer Interactions," The Aeronautical Journal, Vol. 104, No. 3, 2000, pp. 129-140.
21. Schubauer, G. B., and Spangenberg, W. G., "Forced Mixing in Boundary Layers," Journal of Fluid Mechanics, Vol. 8, Pt. 1, 1959, pp. 10-52.
22. McCormick, D. C., "Shock/Boundary-Layer Interaction Control with Vortex Generators and Passive Cavity," AIAA Journal, Vol. 31, No. 1, 1993, pp. 91-96.
23. Stanewsky, E., "Aerodynamic Benefits of Adaptive Wing Technology," Aerospace Science and Technology, Vol. 4, No. 7, 2000, pp. 439-452.