Affiliation:
1. University of Cambridge
Publisher
American Institute of Aeronautics and Astronautics
Reference8 articles.
1. Shock Wave–Boundary-Layer Interactions
2. Shock Wave-Boundary-Layer Interactions in Subsonic Intakes at High Incidence
3. 5COLLISS, S. P., Vortical structures on three-dimensional shock control bumps, PhD Thesis,University of Cambridge, 2014.
Cited by
1 articles.
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