Affiliation:
1. Saint Louis University
Publisher
American Institute of Aeronautics and Astronautics
Reference15 articles.
1. Aircraft Engine Design, Second Edition
2. Warning, S., Design and Exploration of a New Blowdown Wind Tunnel for Studying Shock Wave Boundary Layer Interactions. PhD dissertation, Parks College of Engineering,Aviation, and Technology,Saint Louis University, December 2017.
3. Shock Wave Boundary Layer Interaction Unsteadiness: The Effects of Configuration and Strength
4. Corner separation effects for normal shock wave/turbulent boundary layer interactions in rectangular channels