Dual point redesign of an axial compressor airfoil using a viscous inverse design method

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Department of Mechanical and Industrial Engineering, Concordia University, Montreal, QC H3G 1M8, Canada [1 ]
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Proc. ASME Turbo Expo | / PARTS A, B, AND C卷 / 957-966期
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摘要：
Navier Stokes equations
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