Mitigation of Adverse Effects Caused by Shock Wave Boundary Layer Interactions through Optimal Wall Shaping-Reference-Cited by-同舟云学术

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Mitigation of Adverse Effects Caused by Shock Wave Boundary Layer Interactions through Optimal Wall Shaping

Published:2013-06-22 Issue: Volume: Page:
ISSN:
Container-title:31st AIAA Applied Aerodynamics Conference
language:
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Author:

Liou May-Fun¹,Lee Byung Joon²

Affiliation:

1. NASA Glenn Research Center

2. University of California, Santa Barbara

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-2653

Reference25 articles.

1. M.K. Fukuda, W.R. Hingst, and E. Reshotko, "Control of Shock Wave-Boundary Layer Interactions by BleedinSupersonicMixedCompressionInlets", NASACR-2595,1975.

2. Shock-wave/boundary-layer interactions with bleed through rows of holes

3. Vortex-Generator Installation Studies on Steady-State and Dynamic Distortion

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