What is it about?
Shock boundary layer interactions (SBLIs) are common in high-speed flight. In this paper, we characterize the mean flow and unsteadiness in swept impinging SBLIs. The results help in significantly improving our understanding of the underlying flow physics when encountering three-dimensional geometries.
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This page is a summary of: Experimental Study of Swept Impinging Oblique Shock/Boundary-Layer Interactions, AIAA Journal, January 2021, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j058910.
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