For the thin aerofoil of mean camber line given by:z = f (1+x/b)(1−x/b)with f the maximum camber, find the lift coefficient, thezero lift AOA, the moment coefficient about the leadingedge, the moment coefficient about the aerodynamic centreand the location of the aerodynamic centreConsider a thin symmetric aerofoil at 2° angle of attack.Calculate the lift and the moment about the leading edge.Consider an NACA 2412 aerofoil with a 2-m chord in an air-stream with a velocity of 50m/s at standard sea levelconditions. If the lift per unit span is 1353 N, what is the AOA?

Step 1: Thin Aerofoil Properties:The lift coefficient CL for a thin aerofoil is directly…

Answered: For the thin aerofoil of mean camber…

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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