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The incidence  is simulated by a shearing transformation so that the upper and lower surfaces of the airfoil and are defined by equation (1). Note that x, z and c are nondimensionalized by normalizing each by the chord c. A thin airfoil is represented by a camber line d(x) proportional to dm with d(0)=d(1)=0 and a thickness distribution e(x) proportional to em with e(0)=e(1)=0. Download Thin Airfoil Theory - Project 2 | EAE 127 and more Aerospace Engineering Study Guides, Projects, Research in PDF only on Docsity!EAE 127 Project 2 Thin Airfoil Theory Fall 2008 Due Friday, 10/13 (in drop box C) The objective of this project is to get familiar with the thin-airfoil theory and also the code thinair.f to analyze the inviscid, incompressible, small disturbance flow past thin profiles.