Experimental Investigation of a Cylinder-Induced Transitional Shock Wave-Boundary Layer Interaction

E. L. Lash, Christopher S. Combs, Phillip A. Kreth, John D. Schmisseur
  • January 2017, American Institute of Aeronautics and Astronautics (AIAA)
  • DOI: 10.2514/6.2017-0760
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http://dx.doi.org/10.2514/6.2017-0760

The following have contributed to this page: Dr. Christopher S Combs