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
Platzer, Max Franz Ekaterinaris, J.A.
Naval Postgraduate School (U.S.)
Naval Postgraduate School
M.S. in Aeronautical Engineering
Aeronautics and Astronautics
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