Daniel J. Garmann
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View article: Resolvent analysis of an airfoil laminar separation bubble at Re =\n 500,000
Resolvent analysis of an airfoil laminar separation bubble at Re =\n 500,000 Open
We perform resolvent analysis to examine the perturbation dynamics over the\nlaminar separation bubble (LSB) that forms near the leading edge of a NACA 0012\nairfoil at a chord-based Reynolds number of 500,000 and an angle of attack of 8\n…