Wind-tunnel setup for investigations of normal shock wave/boundary-layer interaction control

AIAA Journal

Volumn 44, Issue 11, 2006, Pages 2803-2805

  Ogawa, H ^a,b,c   Babinsky, H ^a,c,d  

^a UNIVERSITY OF CAMBRIDGE   (United Kingdom)

^b Aerodynamics Laboratory   (United Kingdom)

^c AIAA   (United States)

^d Department of Engineering ^*

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY-LAYER DISPLACEMENT; SHOCK CONTROL; SHOCK INSTABILITY;

NOZZLES; PROBLEM SOLVING; SHOCK WAVES; WIND TUNNELS;

BOUNDARY LAYER FLOW;

EID: 33751229268     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.24370     Document Type: Article

References (12)

1. Délery, J., "Shock Wave/Boundary Layer Interaction and its Control," Progress in Aerospace Sciences, Vol. 22, No. 4,1985, pp. 209-280.
2. Délery, J. and Bur, R., "The Physics of Shock Wave/Boundary Layer Interaction Control: Last Lessons Learned," ONERA TP 2000-181, 2000.
3. Stanewsky, E., "Adaptive Wing and Flow Control Technology," Progress in Aerospace Sciences, Vol. 37, No. 7, 2001, pp. 583-667.
4. Stanewsky, E., Délery, J., Fulker, J., and Geißler, W., EUROSHOCK: Drag Reduction by Passive Shock Control, Notes on Numerical Fluid Mechanics, Vol. 56, Vieweg, Braunschweig/Weisbaden, Germany, 1997.
5. Stanewsky, E., Délery, J., Fulker, J., and de Matteis, P., EUROSHOCK 2: Drag Reduction by Shock and Boundary Layer Control, Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Vol. 80, Springer, Berlin, 2002.
6. Ogawa, H., and Babinsky, H., "Evaluation of Wave Drag Reduction by Flow Control," Aerospace Science and Technology, Vol. 10, No. 1, 2006, pp. 1-8.
7. Holden, H. A., "Transonic Shock/Boundary Layer Interaction Control Using Three-dimensional Devices," Ph.D. Dissertation, University of Cambridge, Cambridge, England, U.K., 2004.
8. Orphanides, M. J., Hafenrichter, E. S., Lee, Y., Dutton, J. C., Loth, E., and Stephen, T. M., "Shock-Position Sensitivity and Performance of SBLI Passive-Control Methods," AIAA Paper 2001-2439, 2001.
9. Srinivasan, K. R., Loth, E., and Dutton, J. C., "Aerodynamics of Recirculating Flow Control Devices for Normal Shock/Boundary Layer Interactions,", AIAA Paper 2004-0426, 2004.
10. Seddon, J., "The Flow Produced by Interaction of a Turbulent Boundary Layer with a Normal Shock of Strength Sufficient to Cause Separation," Aeronautical Research Council (ARC) R&M 3502, U.K., 1960.
11. Kooi, J. W., "Influence of Free-Stream Mach Number on Transonic Shock-Wave Boundary-Layer Interaction," National Aerospace Laboratory (NLR)NLR MP 78013 U, The Netherlands, 1978.
12. Ogawa, H., and Babinsky, H., "Experimental Investigation of 3-D Shock/Boundary Layer Interaction Control in Transonic Flows," AIAA Paper 2006-0879, 2006.