The results of experiments investigating excitation of flow instability over a VR-7 airfoil at a post-stall angle of attack of 19° are presented. The Reynolds number based on the chord… Click to show full abstract
The results of experiments investigating excitation of flow instability over a VR-7 airfoil at a post-stall angle of attack of 19° are presented. The Reynolds number based on the chord was fixed at...
               
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