Effect of height of microvortex generators on swept shock wave boundary layer interactions
Author:
Publisher
Springer Science and Business Media LLC
Subject
Aerospace Engineering,Transportation
Link
http://link.springer.com/content/pdf/10.1007/s13272-013-0075-y.pdf
Reference23 articles.
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3. Barnhart, P.J., Greber, I., Hingst, W.R.: Glancing shock wave turbulent boundary layer interaction with boundary layer suction. In: AIAA Paper 88-0308 (1988)
4. Gaitonde, D., Knight, D.: Numerical investigation of some control methods for 3-d turbulent interactions due to sharp fins. In: 27th Aerospace Sciences Meeting, Reno, Nevada, AIAA Paper 89-0360, January, pp. 1–20 (1989)
5. Gaitonde, D., Knight, D.: Numerical investigation of bleed on three-dimensional turbulent interactions due to sharp fins. AIAA J. 11(29), 1878–1885 (1991)
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