1 ;ioyalAircraftEstablkhme I

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Date: 2013-12-05 07:25:35 Fluid dynamics Dynamics Boundary layer Airfoil Drag Shock wave Wind tunnel Turbulence Mach number Aerodynamics Aerospace engineering Fluid mechanics		1 ;ioyalAircraftEstablkhme I Add to Reading List Source URL: naca.central.cranfield.ac.uk Download Document from Source Website File Size: 4,35 MB Share Document on Facebook

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