NASA Technical Reports Server (NTRS) 19790011874: Wake curvature and trailing edge interaction effects in viscous flow over airfoilsReport as inadecuate



 NASA Technical Reports Server (NTRS) 19790011874: Wake curvature and trailing edge interaction effects in viscous flow over airfoils


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A theory developed for analyzing viscous flows over airfoils at high Reynolds numbers is described. The theory includes a complete treatment of viscous interaction effects induced by the curved wake behind the airfoil and accounts for normal pressure gradients across the boundary layer in the trailing edge region. A brief description of a computer

Author: NASA Technical Reports Server (NTRS)

Source: https://archive.org/







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