Evaluation of wave drag reduction by flow control

43rd AIAA Aerospace Sciences Meeting and Exhibit - Meeting Papers

Volumn , Issue , 2005, Pages 5519-5528

  Ogawa, H ^a,b   Babinsky, H ^a,b  

^a UNIVERSITY OF CAMBRIDGE   (United Kingdom)

^b AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; FLOW CONTROL; SHOCK WAVES; TRANSONIC AERODYNAMICS;

SHOCK CONTROL; SHOCK STRUCTURE; TRANSONIC AEROFOILS; WAVE DRAG;

DRAG;

EID: 30744466435     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-1415     Document Type: Conference Paper

References (19)

1. Délery,J., and Bur,R., "The physics of shock wave / boundary layer interaction control: last lessons learned", ECCOMASS 2000, Barcelona, 2000
2. Stanewsky,E., Délery,J., Fulker,J.L. and Wolfgang,G., "EUROSHOCK - Drag Reduction by Passive Shock Control", Noteson Numerical Fluid Mechanics, vol.56, 1997
3. Holden,H.A. and Babinsky,H., "Controlling A Separated Shock / Boundary Layer Interaction Using Streamwise Slots At Mach 1.5" to be published by Journal of Aircraft, 2004
4. Smith,A.N., Babinsky,H., Dhanasekaran,P.C., Savill,A.M. and Dawes,W.N., "Computational Investigation of Groove Controlled Shock Wave / Boundary Layer Interaction", AIAA Paper 2003-0446, 2003
5. Loth,E., Jaiman,R., Button,C.,White, S.,Roos, F.,Mace,J. and Davis,D., "Mesoflap and Bleed Flow Control for a Mach 2 Inlet", AIAA Paper 2004-0855, 2004
6. Smith,B.L. and Glezer,A., "The formation and evolution of synthetic jets", Physics of Fluids, vol.10, No.9, 1998, pp.2281-2297
7. Stanewsky,E., Delery,J., Fulker,J.L. and de Matteis,P., "EUROSHOCK II - Drag Reduction by Shock and Boundary Layer Control", Notes on Numerical Fluid Mechanics and Multidisciplinary Design, vol.80, 2002
8. Smith,A.N., Holden,H.A., Babinsky,H., Fulker,J.L. and Ashil,P.R., "Control of Normal Shock Wave / Turbulent Boundary Layer Interactions Using Streamwise Grooves", AIAA 2002-0978, 2002
9. Lock,R.C.,"The prediction of the drag of aerofoils and wings at high subsonic speeds", RAE TM Aero 2044, 1985
10. ESDU International Ltd., "VGK method for two-dimensional aerofoil sections. Parti: principles and results.", ESDU 96028, 1996
11. von Neumann,J., Collected Works, vol.6, Pergamon, New York, 1963
12. Hornung,H., "Regular and Mach reflection of shock waves", Annual Review of Fluid Mechanics, 1986
13. Dargel,G. and Thiede P., "Assessment of Shock and Boundary Layer Control Concepts for Hybrid Laminar Flow Wing Design", Notes on Numerical Fluid Mechanics and Multidisciplinary Design, vol.80, 2002, pp.383-414
14. Tesdall,A.M. and Hunter,J.K., "Self-similar solutions for weak shock reflection", Journal of Applied Mathematics, vol.63, No.1, 2002, pp.42-61
15. Szwaba,R., Doerffer,P., Namieśnik,K. and Szulc,O., "Flow structure in the region of three shock wave interaction", Aerospace Science and Technology, vol.8, 2004, pp.499-508
16. Kobayashi,S. and Adachi,T., "Nonself-simular behavior of the von Neumann reflection", Physics of Fluids, vol.12, No.7, 2000, pp.1869-1877
17. Bleakney,W. and Taub,A.H., "Interaction of shock waves", Review of Modern Physics, vol.21, 1949, pp.584-605
18. Sternberg,J., "Triple-shock-wave intersections", Physics of Fluids, vol.2, 1959, pp.179-206
19. Sasoh,A., Takayama,T. and Saito,T., "A weak shock wave reflection over wedges", Shock Waves, vol.2, 1993, pp.277-281