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Grid Dependency Study for the NASA Rotor 37 Compressor Blade. ASME 1997 International Gas Turbine and Aeroengine Congress and Exhibition. 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery:pp.V001T03A056;(9pages).
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Numerical Prediction of Trailing Edge Wake Shedding. ASME Turbo Expo. 
June 2–5, Orlando, FL, USA, ASME paper 97-GT-89