![]() Once you master these principles, you’ll never look at an aircraft the same. Airfoil analysis and design is fascinating and exciting. Van Buren 2.25K subscribers This lecture covers Thin Airfoil Theory, which represents a completion of all the theoretical work we've done up to this point. Since the airfoil is thin, x (chord position) can be used instead of s, and all angles can be approximated as small. By the Kutta condition, the vorticity is zero at the trailing edge. The mean-line, y (x), is considered to produce a distribution of vorticity along the line, s. 1, lets look at the lift curve comparison. The airfoil is modeled as a thin lifting mean-line (camber line). ![]()
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