Preliminary Unsteady Characterization of Shock Wave/Boundary Layer Interactions on a 4% Scale SLS Model using uPSP and Shadowgraph
Author:
Affiliation:
1. University of Tennessee, Tullahoma
2. NASA Ames Research Center
Publisher
American Institute of Aeronautics and Astronautics
Reference20 articles.
1. A review of aerothermal problems associated with hypersonic flight
2. Progress in shock wave/boundary layer interactions
3. Progress on the launch-vehicle buffeting problem
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