What is it about?
PSP visualization and analysis of laminar boundary layer - Shockwave interactions on a NACA 0012 airfoil.
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Why is it important?
The airflow conditions of this experiment are unusual. The flow is mostly laminar, but in a transonic regime.
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This page is a summary of: Experimental study of shock wave patterns over an airfoil, June 2016, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/6.2016-3935.
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