ME 488 - North Dakota State University -ME 488/688 - Homework #5
ME 488/688 - HW #5 Due Date: Friday 11/10/2017 Finite Wing Problem 1. The measured lift slope for the NACA 23012 airfoil is 0.1080 per degree, and the zero-lift angle is
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me 488 north dakota state university me 488688 homework 5