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Date: 2014-06-16 15:21:24Fluid 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. 6Add to Reading ListSource URL: history.arc.nasa.govDownload Document from Source WebsiteFile Size: 1,28 MBShare Document on Facebook |
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