Transition prediction of a hypersonic boundary layer over a cone at small angle of attack—with the improvement of e N method-Reference-Cited by-同舟云学术

Transition prediction of a hypersonic boundary layer over a cone at small angle of attack—with the improvement of e N method

Published:2009-01 Issue:1 Volume:52 Page:115-123
ISSN:1672-1799
Container-title:Science in China Series G: Physics, Mechanics and Astronomy
language:en
Short-container-title:Sci. China Ser. G-Phys. Mech. Astron.

Author:

Su CaiHong,Zhou Heng

Publisher

Springer Science and Business Media LLC

Link

http://link.springer.com/content/pdf/10.1007/s11433-009-0006-4.pdf

Reference17 articles.

1. Low G M. Boundary-layer transition at supersonic speeds. NACA RM E56E10. 1956

2. Stetson K F, Thompson E R, Donaldson J C, et al. Laminar boundary layer stability experiments on a cone at Mach 8. III-Sharp cone at angle of attack. AIAA Paper. Washington: AIAA, 85-0492

3. Doggett G P, Chokani N, Wilkinson S P. Effect of angle of attack on hypersonic boundary-layer stability. AIAA J, 1997, 35(3): 464–470

4. Stetson K F. Hypersonic boundary layer transition experiments. AFWAL-TR-80-3062. 1980

5. Fischer M C, Rudy D H. Effect of angle of attack on boundary-layer transition at Mach 21. AIAA J, 1971, 9(6): 1203–1205

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