Simulation of three-dimensional symmetric and asymmetric instabilities in attachment-line boundary layers

AIAA Journal

Volumn 34, Issue 11, 1996, Pages 2432-2434

  Joslin, Ronald D ^a,b  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b AIAA ^*

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0013017378     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.13415     Document Type: Article

References (18)

1. Cumpsty, N. A., and Head, M. R., "The Calculation of the Three-Dimensional Turbulent Boundary Layer. Part III. Comparison of Attachment-Line Calculations with Experiment," Aeronautical Quarterly, Vol. 20, May 1969, pp. 99-113.
2. Pfenninger, W., and Bacon, J. W., Jr., "Amplified Laminar Boundary-Layer Oscillations and Transition at the Front Attachment Line of a 45 Degree Swept Flat-Nosed Wing With and Without Boundary-Layer Suction," Viscous Drag Reduction, edited by C. S. Wells, Plenum, New York, 1969, pp. 85-105.
3. Poll, D. I. A., "Transition in the Infinite Swept Attachment Line Boundary Layer," Aeronautical Quarterly, Vol. 30, Nov. 1979, pp. 607-628.
4. Poll, D. I. A., "Three-Dimensional Boundary Layer Transition via the Mechanisms of Attachment-Line Contamination and Crossflow Stability," Laminar-Turbulent Transition, edited by R. Eppler and H. Fasel, Springer, Stuttgart, Germany, 1980, pp. 253-262.
5. Hall, P., Malik, M. R., and Poll, D. I. A., "On the Stability of an Infinite Swept Attachment Line Boundary Layer," Proceedings of the Royal Society of London, Series A: Mathematical and Physical Science, Vol. 395, Oct. 1984, pp. 229-245.
6. Spalart, P. R., "Direct Numerical Study of Leading-Edge Contamination," AGARD, CP-438, 1989, pp. 5.1-5.13.
7. Theofilis, V., "Numerical Experiments on the Stability of Leading Edge Boundary Layer Flow: A Two-Dimensional Linear Study," International Journal for Numerical Methods in Fluids, Vol. 16, Jan. 1993, pp. 153-170.
8. Jiménez, J., Martel, C., Agüi, J. C., and Zufiria, J. A., "Direct Numerical Simulation of Transition in the Incompressible Leading Edge Boundary Layer," ETSIA/MF-903, Universidad Politecnica Madrid, Spain, 1990.
9. Joslin, R. D., "Direct Simulation of Evolution and Control of Nonlinear Instabilities in Attachment-Line Boundary Layers," AIAA Paper 94-0826 Jan. 1994.
10. Joslin, R. D., "Direct Simulation of Evolution and Control of Three-Dimensional Instabilities in Attachment-Line Boundary Layers," Journal of Fluid Mechanics, Vol. 291, May 1995, pp. 369-392.
11. Pfenninger, W., "Flow Phenomena at the Leading Edge of Swept Wings," Recent Developments in Boundary Layer Research, AGARD 97, May 1965.
12. Gregory, N., and Love, E. M., "Laminar Flow on a Swept Leading Edge," National Physical Lab., Final Progress Rept., NPL Aero. Memo., Vol. 26, Oct. 1965.
13. Gaster, M., "On the Flow Along Swept Leading Edges," Aeronautical Quarterly, Vol. 18, May 1967, pp. 165-184.
14. Poll, D. I. A., "Some Observations of the Transition Process on the Windward Face of a Long Yawed Cylinder," Journal of Fluid Mechanics, Vol. 150, Jan. 1985, pp. 329-356.
15. Hall, P., and Malik, M. R., "On the Instability of a Three-Dimensional Attachment-Line Boundary Layer: Weakly Nonlinear Theory and a Numerical Simulation," Journal of Fluid Mechanics, Vol. 163, Feb. 1986, pp. 257-282.
16. Lin, R.-S., and Malik, M. R., "The Stability of Incompressible Attachment-Line Boundary Layers - A 2D-Eigenvalue Approach," AIAA Paper 94-2372, June 1994.
17. Lin, R.-S., and Malik, M. R., "Stability and Transition in Compressible Attachment-Line Boundary-Layer Flow," Aerotech '95, Society of Automotive Engineers, SAE Paper 952041, Los Angeles, CA, Sept. 1995.
18. Fedorov, S., personal communication, Moscow Inst. of Physics and Technology, Zhukovsky, Russia, 1995.