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<p>Steady and unsteady two-dimensional flowfield analysis was conducted for a Sikorsky SSC-AO9 airfoil in compressible, high Reynolds number flows. Limited verification with experimental measurement was achieved. Computational methods included a steady, line
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<br>Subjects: Dynamic Stall; Supercritical Airfoil; Navier-Stokes Solution; Shock-induced Boundary Layer Separation</div>
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Johnston, Thomas A.</div>
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