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Fluid dynamics / Lift / Airfoil / Shock wave / Boundary layer / Pressure coefficient / Mach number / Computational fluid dynamics / Stall / Aerodynamics / Aerospace engineering / Fluid mechanics


564 AIAA JOURNAL VOL. 16, NO. 6
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Document Date: 2014-06-16 15:21:24

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File Size: 1,28 MB

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