Experimental and Computational Investigations of Shock Wave – Boundary Layer Interaction on a Transonic Airfoil with and without Bump | AVESİS

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Experimental and Computational Investigations of Shock Wave – Boundary Layer Interaction on a Transonic Airfoil with and without Bump

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MALKOÇOĞLU U. E., BARADA M. E. H. A., ÇETİN F., ÇELİK B., YÜCEİL K. B.

AIAA AVIATION 2020 FORUM, VIRTUAL EVENT, United States Of America, 15 - 19 June 2020

Publication Type: Conference Paper / Full Text
Doi Number: 10.2514/6.2020-2759
City: VIRTUAL EVENT
Country: United States Of America
Istanbul Technical University Affiliated: Yes