Interactions between shock waves and turbulent boundary layers-Reference-Cited by-同舟云学术

Interactions between shock waves and turbulent boundary layers

Published:1970-01 Issue: Volume:11 Page:235-340
ISSN:0376-0421
Container-title:Progress in Aerospace Sciences
language:en
Short-container-title:Progress in Aerospace Sciences

Author:

Green J.E.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Aerospace Engineering

Reference78 articles.

1. On the hypersonic laminar near wake critical point of the Crocco-Lees mixing theory;Ai;AIAA Paper No. 67-60,1967

2. Integral theory for supersonic turbulent base flows;Alber;AIAA J.,1968

3. Separation of a supersonic turbulent boundary layer;Bogdonoff;J. Aero. Sci.,1955

4. Calculation of boundary layer development using the turbulent energy equation II: compressible flow on adiabatic walls;Bradshaw;NPL Aero Rep. 1217,1966

5. Investigation of separated flows in supersonic and subsonic streams with emphasis on the effect of transition;Chapman;NACA TN 3869, NACA Rep. 1356,1957

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