Three dimensional shock wave turbulent boundary layer interactions -A parametric study of blunted fin-induced flows-Reference-Cited by-同舟云学术

Three dimensional shock wave turbulent boundary layer interactions -A parametric study of blunted fin-induced flows

Published:1978-01-16 Issue: Volume: Page:
ISSN:
Container-title:16th Aerospace Sciences Meeting
language:
Short-container-title:

Author:

DOLLING D.¹,BOGDONOFF S.¹

Affiliation:

1. Princeton University, Princeton, N.J.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1978-159

Reference7 articles.

1. I. E. "Study of Three-Dimensional Flow Fields Generated by the Interaction of a Skewed Shock Wave with a Turbulcnt Boundary Layer', AFFLI!. TR-75-21, February 1975.

2. Oskam, B. "Three-DimensionalFlow Fields Generated by the Interaction of a Swept Shock Wave with a Turbulent Boundary Layer", Ph.D. Thesis,Dept. of Aerospace and Mechanical Sciences, Princeton University, 1976. 4. Vas, I.E., and Bogdonoff, 5. M. "A

Cited by 6 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. A re-examination of the upstream influence scaling and similarity laws for 3-D shock wave/turbulent boundary layer interactions;24th Aerospace Sciences Meeting;1986-01-06

2. Blunt fin-induced shock wave/turbulent boundary-layer interaction;AIAA Journal;1982-12

3. An experimental investigation of the unsteady behavior of blunt fin-induced shock wave turbulent boundary layer interaction;14th Fluid and Plasma Dynamics Conference;1981-06-23

4. Analysis of Weak Glancing Shock/Boundary-Layer Interactions;Journal of Aircraft;1980-03

5. Detailed Study of Attached and Separated Compression Corner Flowfields in High Reynolds Number Supersonic Flow;AIAA Journal;1979-06