Evaluation of wave drag reduction by flow control

Aerospace Science and Technology

Volumn 10, Issue 1, 2006, Pages 1-8

  Ogawa, H ^a   Babinsky, H ^a  

^a UNIVERSITY OF CAMBRIDGE   (United Kingdom)

Author keywords

shock structure; Flow control; Prediction; Transonic aerofoil; Wave drag

Indexed keywords

AIRFOILS; COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; DRAG; FLOW CONTROL; VIBRATIONS (MECHANICAL); WINGS;

Λ-SHOCK STRUCTURE; PREDICTION; TRANSONIC AEROFOIL; WAVE DRAG;

AERODYNAMICS;

EID: 31044452879     PISSN: 12709638     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ast.2005.08.001     Document Type: Article

References (19)

1. W. Bleakney, and A.H. Taub Interaction of shock waves Rev. Modern Phys. 21 1949 584 605
2. G. Dargel, and P. Thiede 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 383 414
3. J. Délery, R. Bur, The physics of shock wave/boundary layer interaction control: last lessons learned, in: ECCOMASS 2000, Barcelona, 2000
4. H.A. Holden, and H. Babinsky Separated shock-boundary-layer interaction control using streamwise slots J. Aircraft 42 1 2005 166 171
5. H.A. Holden, H. Babinsky, Shock/boundary layer interaction control using 3D devices, AIAA Paper 2003-0447, 2003
6. S. Kobayashi, and T. Adachi Nonself-simular behavior of the von Neumann reflection Phys. Fluids 12 7 2000 1869 1877
7. R.C. Lock, The prediction of the drag of aerofoils and wings at high subsonic speeds, RAE TM Aero 2044, 1985
8. E. Loth, R. Jaiman, C. Dutton, S. White, F. Roos, J. Mace, D. Davis, Mesoflap and bleed flow control for a Mach 2 inlet, AIAA Paper 2004-0855, 2004
9. H. Ogawa, H. Babinsky, Evaluation of wave drag reduction by flow control, AIAA Paper 2005-1415, 2005
10. A. Sasoh, T. Takayama, and T. Saito A weak shock wave reflection over wedges Shock Waves 2 1993 277 281
11. A.N. Smith, H. Babinsky, P.C. Dhanasekaran, A.M. Savill, W.N. Dawes, Computational investigation of groove controlled shock wave/boundary layer interaction, AIAA Paper 2003-0446, 2003
12. A.N. Smith, H. Babinsky, J. Fulker, and P.R. Ashill Shock-wave/boundary- layer interaction control using streamwise slots in transonic flows J. Aircraft 41 3 2004 540 546
13. A.N. Smith, H.A. Holden, H. Babinsky, J.L. Fulker, P.R. Ashil, Control of normal shock wave/turbulent boundary layer interactions using streamwise grooves, AIAA Paper 2002-0978, 2002
14. B.L. Smith, and A. Glezer The formation and evolution of synthetic jets Phys. Fluids 10 9 1998 2281 2297
15. E. Stanewsky, J. Délery, J.L. Fulker, and P. de Matteis EUROSHOCK II - Drag Reduction by Shock and Boundary Layer Control Notes on Numerical Fluid Mechanics and Multidisciplinary Design vol. 80 2002
16. E. Stanewsky, J. Délery, J.L. Fulker, and G. Wolfgang EUROSHOCK - Drag Reduction by Passive Shock Control Notes on Numerical Fluid Mechanics vol. 56 1997
17. J. Sternberg Triple-shock-wave intersections Phys. Fluids 2 1959 179 206
18. R. Szwaba, P. Doerffer, K. Namieśnik, and O. Szulc Flow structure in the region of three shock wave interaction Aerospace Science and Technology 8 2004 499 508
19. A.M. Tesdall, and J.K. Hunter Self-similar solutions for weak shock reflection J. Appl. Math. 63 1 2002 42 61