Assessment of shock induced flow separation and mixing layer predictions in nozzles and high speed jets-Reference-Cited by-同舟云学术

Assessment of shock induced flow separation and mixing layer predictions in nozzles and high speed jets

Published:2001-01-08 Issue: Volume: Page:
ISSN:
Container-title:39th Aerospace Sciences Meeting and Exhibit
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Author:

Hamed Awatef¹,Mohamed Ashraf¹

Affiliation:

1. Cincinnati, Univ., OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2001-225

Reference22 articles.

1. Survey of validation data base for shockwave boundary-layer interactions in supersonic inlets

2. Flow Separation in Shock Wave Boundary Layer Interactions

3. Hunter, C. A. "An experimental Analysis of Passive Shock Boundary Layer Interaction Control for Improving the Off-Design Performance of Jet Exhaust Nozzles," M.S. Thesis,George Washington Univ., Washington, DC, Sept. 1993.

4. Garrard, G., Phares, W., and Cooper, G. "Calibration of PARC for Propulsion Flows",June 1991.

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