564 AIAA JOURNAL VOL. 16, NO. 6

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Date: 2014-06-16 15:21:24 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 Add to Reading List Source URL: history.arc.nasa.gov Download Document from Source Website File Size: 1,28 MB Share Document on Facebook

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