The effects of expansions on a supersonic boundary layer - Surface pressure measurements-Reference-Cited by-同舟云学术

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The effects of expansions on a supersonic boundary layer - Surface pressure measurements

Published:1994-01-10 Issue: Volume: Page:
ISSN:
Container-title:32nd Aerospace Sciences Meeting and Exhibit
language:
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Author:

Dawson Jonathan¹,Samimy Mo¹

Affiliation:

1. Ohio State Univ., Columbus

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1994-648

Reference34 articles.

1. The effect of mean compression or dilatation on the turbulence structure of supersonic boundary layers

2. The Response of Turbulent Boundary Layers to Sudden Perturbations

3. Spina, E. F., Smits, A. J., and Robinson, S. K. "ThePhysicsof SupersonicTurbulentBoundary Layers," to appear in Annual Review of Fluid Mechanics, 1994.

4. Willmarth, W.W. "Pressure Fluctuations Beneath Turbulent Boundary Layers,'I Annual ReviewofFluidMechanics, Vol.7, 1975,pp.13-38.

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Effect of a rapid expansion on the development of compressible free shear layers;Fluid Dynamics Conference;1994-06-20

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