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[American Institute of Aeronautics and Astronautics AIAA AVIATION 2020 FORUM - VIRTUAL EVENT ()] AIAA AVIATION 2020 FORUM - Exploration of Upstream Influence and the Role of Shock Generator Geometry in Shock Wave/Transitional Boundary Layer Interactions at Mach 1.8 Edge Conditions
Lash, E. Lara, Gragston, Mark, McDaniel, Zachary, Kreth, Phillip A., Schmisseur, John D.DOI:
10.2514/6.2020-2999
File:
PDF, 1.44 MB