Aerodynamic heating in the region of shock and turbulent boundary layer interaction induced by a cylinder-Reference-Cited by-同舟云学术

Aerodynamic heating in the region of shock and turbulent boundary layer interaction induced by a cylinder

Published:1992-08 Issue:3 Volume:8 Page:224-230
ISSN:0567-7718
Container-title:Acta Mechanica Sinica
language:en
Short-container-title:Acta Mech Sinica

Author:

Guiming Tang,Hongru Yu

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Computational Mechanics

Link

http://link.springer.com/content/pdf/10.1007/BF02489245.pdf

Reference15 articles.

1. Войженко Д. М., и другие, Обтекание Цилиндрилеского препятетвия на пластина сверхзвуковыи потоком гаэа, и эв,Акад, Наук, СССР Механука Зидкости и 2a3a, 1 (1966)

2. Westkaemper JC. Turbulent boundary layer separation ahead cylinder, AIAA J, 1968, 6 (7)

3. Sedney R & Kitchens, C W Jr Separation ahead protuberance in supersonic turbulent boundary layer. AIAA J, 1977, 15 (4)

4. Kaufman L G et al. Shock impingement caused by boundary layer separation ahead of blunt fins. AIAA J, 1973, 11(10)

5. Halpin R N. Step induced boundary layer separation phenomena. AIAA J, 1965, 3(3)

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