Preliminary Investigation Into the Effects of Cross-Flow on Low Reynolds Number Transition

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Date: 2011-09-07 13:54:26 Fluid dynamics Boundary layer Tollmien–Schlichting wave Airfoil Laminar flow Lift Reynolds number Navier–Stokes equations Swept wing Aerodynamics Aerospace engineering Fluid mechanics		Preliminary Investigation Into the Effects of Cross-Flow on Low Reynolds Number Transition Add to Reading List Source URL: raphael.mit.edu Download Document from Source Website File Size: 3,14 MB Share Document on Facebook

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