On the Effect of Test Section Aspect Ratio for Shock Wave - Boundary Layer Interactions
Author:
Affiliation:
1. Saint Louis University
2. The Boeing Company
3. Air Force Research Laboratory
4. University of Cambridge
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2017-0535
Reference25 articles.
1. Shock Wave–Boundary-Layer Interactions
2. Progress in shock wave/boundary layer interactions
3. 3Norby, W., Ladd, J., and Yuhas, A. "Dynamic Inlet Distortion Prediction with a Combined Computational Fluid Dynamics and Distortion Synthesis Approach," NASA Contractor Report 198053, 1996.
4. A review of the use of vortex generators for mitigating shock-induced separation
5. Experimental investigation into Parameters Governing Corner Interactions for Transonic Shock-Wave/Boundary-Layer Interactions
Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Numerical Simulation of Sidewall Influence on Supersonic Compression Ramp Interactions;2018 Fluid Dynamics Conference;2018-06-24
2. Shock-Wave/Boundary-Layer Interaction in a Large-Aspect-Ratio Test Section;AIAA Journal;2017-09
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