Experimental Study into the Effects of Forced Transition on a Shock-Wave/Boundary-Layer Interaction-Reference-Cited by-同舟云学术

Experimental Study into the Effects of Forced Transition on a Shock-Wave/Boundary-Layer Interaction

Published:2016-04 Issue:4 Volume:54 Page:1313-1325
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Giepman Rogier H. M.¹,Louman Renee¹,Schrijer Ferry F. J.¹,van Oudheusden Bas W.¹

Affiliation:

1. Delft University of Technology, 2629 HS Delft, The Netherlands

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J054501

Reference23 articles.

1. Fifty Years of Shock-Wave/Boundary-Layer Interaction Research: What Next?

2. Shock Wave–Boundary-Layer Interactions

3. ChapmanD. R.KuehnD. M.LarsonH. K. “Investigation of Separated Flows in Supersonic and Subsonic Streams with Emphasis on the Effect of Transition,” NACA Rept. 1356, 1957.

4. Low-Frequency Unsteadiness of Shock Wave/Turbulent Boundary Layer Interactions

5. Transition location effects on normal shock wave--boundary layer interactions

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