Crossflow instabilities - Theory & technology

41st Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2003, Pages

  Saric, William S ^a   Reed, Helen L ^a  

^a Arizona State University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 78149452561     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (55)

1. Arnal D. 1984. Description and prediction of transition in two-dimensional incompressible flow. AGARD Rep. No. 709 (Special course on stability and transition of laminar flows), Von Karman Inst., Rhode-St.-Genese, Belg.
2. Arnal D. 1992. Boundary-layer transition: Prediction, application to drag reduction. AGARD Rep. No. 786 (Special course on skin friction drag reduction), Von Karman Inst., Rhode-St.-Genese, Belg.
3. Arnal D. 1997. Laminar-turbulent transition: Research and applications in France. AIAA Pap. No. 97-1905
4. Balakumar P, Reed HL. 1991. Stability of threedimensional supersonic boundary layers. Phys. Fluids A 3 (4): 617-32
5. Bippes H. 1997. Environmental conditions and transition prediction in 3-D boundary layers. AIAA Pap. No. 97-1906
6. Bippes H. 1999. Basic experiments on transition in three-dimensional boundary layers dominated by crossflow instability. Prog. Aero. Sci. 35(4):363-412
7. Bushnell DM, Malik MR. 1987. Supersonic laminar flow control. NASA CP-2487
8. Bushnell DM, Tuttle MH. 1979. Survey and bibliography on attainment of laminar flow control in air using pressure gradient and suction. NASA RP 1035, 1.
9. Collier FS Jr. 1993. An overview of recent subsonic laminar flow control flight experiments. AIAA Pap. No. 93-2987
10. Crouch JD. 1997. Transition prediction and control for airplane applications. AIAA Pap. No. 97-1907
11. Dagenhart JR, Saric WS. 1999. Crossflow stability and transition experiments in swept-wing flow. NASA TP 1999-209344
12. Deyhle H, Bippes H. 1996. Disturbance growth in an unstable three-dimensional boundary layer and its dependence on initial conditions. J. Fluid Mech. 316:73-113
13. Duck PW, Hall P. (eds.) 1996. IUTAM Symposium on Nonlinear Instability and Transition in Three-Dimensional Boundary Layers, Amsterdam: Kluwer. 436pp.
14. Fischer MC, Wright AS Jr, Wagner RD. 1983. A flight test of laminar flow control leading-edge systems. NASA TM 85712
15. Gladden RD. 2001. Crossflow transition in elevated freestream turbulence. M.S. Thesis, Arizona State University, December
16. Haynes TS, Reed HL. 2000. Simulation of swept-wing vortices using nonlinear parabolized stability equations. J. Fluid Mech. 405:325-49
17. Herbert, T. 1997a. Parabolized stability equations. Ann. Rev. Fluid Mech. 29:245-83
18. Herbert T. 1997b. Transition prediction and control for airplane applications. AIAA Pap. No. 97-1908
19. Janke E, Balakumar P. 2000. On the secondary instability of three-dimensional boundary layers. Theoret. Comput. Fluid Dyn. 14:167-94
20. Joslin RD. 1998. Aircraft laminar flow control. Ann. Rev. Fluid Mech. 30: 1-29
21. Kachanov YS. 1996. Experimental studies of threedimensional instability of boundary layer. AIAA Pap. No. 96-1976
22. Kawakami M, Kohama Y, Okutsu M. 1999. Stability characteristics of stationary crossflow vortices in three-dimensional boundary layer. AIAA Pap. No. 99-0811
23. Kohama Y, Saric WS, Hoos JA. 1991. A highfrequency, secondary instability of crossflow vortices that leads to transition. In Proc. Royal Aero. Soc. Conf. on Boundary-Layer Transition and Control
24. Lekoudis SG. 1980. Stability of the boundary layer on a swept wing with wall cooling. AIAA J. 18: 1029
25. Mack LM. 1980. On the stabilization of threedimensional boundary layers by suction and cooling. In Laminar-Turbulent Transition, ed. R. Eppler, H. Fasel, pp. 223-38. Berlin: Springer-Verlag
26. Mack LM. 1981. Compressible boundary layer stability calculations for sweptback wings with suction. AIAA J. 20: 363-69
27. Mack LM. 1984. Boundary-layer linear stability theory. In Special Course on Stability and Transition of Laminar Flows, AGARD Report709, pp. 31-81
28. Maddalon DV, Braslow AL. 1990. Simulated-airlineservice flight tests of laminar-flow control with perforated-surface suction system. NASA TP 2966
29. Malik MR, Li F, Chang CL. 1994. Crossflow disturbances in three-dimensional boundary layers: Nonlinear development, wave interaction and secondary instability. J. Fluid Mech. 268:1-36
30. Malik MR, Li F, Chang CL. 1996. Nonlinear crossflow disturbances and secondary instabilities in sweptwing boundary layers See Duck and Hall 1996, pp. 257-66
31. Malik MR, Li F, Choudhari MM, Chang CL. 1999. Secondary instability of crossflow vortices and swept-wing boundary layer transition. J. Fluid Mech. 399:85-115
32. Parikh P. 2003. Active laminar flow control technologies-a review. AIAA Pap. No. 2003-0773.
33. Pfenninger W. 1977. Laminar flow control-Laminarization. AGARD Rep. No. 654 (Special course on drag reduction), Von Karman Inst., Rhode-St.-Genese, Belg.
34. Pfenninger W, Reed HL, Dagenhart JR. 1980. Design considerations of advanced supercritical low drag suction airfoils. Viscous Flow Drag Reduction, AIAA Prog. Astronautics and Aeronautics Ser., 72.
35. Poll DIA. 1985. Some observations of the transition process on the windward face of a long yawed cylinder. J. Fluid Mech. 150:329-56
36. Radeztsky RH Jr, Reibert MS, Saric WS. 1999. Effect of isolated micron-sized roughness on transition in swept-wing flows. AIAA J. 37(11):1371-7
37. Reed HL, Saric WS. 1989. Stability of threedimensional boundary layers. Ann. Rev. Fluid Mech. 21:235-84
38. Reed HL, Saric WS, Arnal D. 1996. Linear stability theory applied to boundary layers. Ann. Rev. Fluid Mech. 28:389-428
39. Reed HL, Saric WS, Haynes TS. 1998 CFD validation issues in transition modeling. AIAA J. 36 (5) 742-51.
40. Reibert MS, Saric WS, Carrillo RB Jr, Chapman KL. 1996. Experiments in nonlinear saturation of stationary crossflow vortices in a swept-wing boundary layer. AIAA Pap. No. 96-0184
41. Reibert MS, Saric WS. 1997 Review of swept-wing transition. AIAA Paper 97-1816.
42. Reshotko E. 1997. Progress, accomplishments and issues in transition research. AIAA Pap. No. 97-1815
43. Saric WS. 1992. Laminar-turbulent transition: Fundamentals. AGARD Rep. No. 786 (Special course on skin friction drag reduction), Von Karman Inst., Rhode-St.-Genese, Belg.
44. Saric WS. 1994a. Görtler vortices. Ann. Rev. Fluid Mech. 26:379-409
45. Saric WS. 1994b. Physical description of boundarylayer transition: Experimental evidence. AGARD Rep. No. 793 (Special course on progress in transition modelling), Von Karman Inst., Rhode-St.-Genese, Belg.
46. Saric WS, Carrillo RB Jr, Reibert MS. 1998a. Nonlinear stability and transition in 3-D boundary layers. Meccanica 33, 469-87
47. Saric WS, Carrillo RB, Reibert MS. 1998b. Leadingedge roughness as a transition control mechanism. AIAA Pap. No. 98-0781
48. Saric WS, Gladden R, Gabet P, White EB. 2000. Control of transition in 3-D boundary layers with streamwise vortices in the presence of freestream turbulence and random surface roughness. Proc. Workshop on Organized Vortical Motion as a Basis for Boundary Layer Control, Ukrainian Academy of Sciences, September 20-22.
49. Saric WS, Reed HL. 2002a. Supersonic laminar flow control on swept wings using distributed roughness. AIAA Pap. No. 2002-0147
50. Saric WS, Reed HL. 2002. Control of transition in supersonic boundary layers: experiments and computations. Keynote Paper, ASME FEDSM-2002-31258, Montreal, July
51. Saric WS, Reed HL, White EB. 2003. Stability of threedimensional boundary layers. Ann. Rev. Fluid Mech. 35
52. Schrauf G, Bieler H, Thiede P. 1992. Transition prediction-the Deutsche Airbus View. Proceedings of the First European Forum on Laminar Flow Technology, Hamburg, DGLR-Bericht 92-06: 73-82
53. von Doenhoff AE, Braslow AL. 1961. The effect of distributed roughness on laminar flow. In Boundary-Layer Control (ed. Lachmann), vol. 2. New York: Pergamon Press, pp. 657-81
54. Wasserman P, Kloker, M. 2002. Mechanisms and control of crossflow-vortex induced transition in a 3-D boundary layer. J. Fluid Mech. 456:49-84
55. White EB, Saric WS. 2003. Secondary instability of crossflow vortices. In press J. Fluid Mech.