Question 1a) The mean camber line of an aerofoil is defined by the relations:mXX x2qC с сxZc =mс(1-9)² |->q.In the above, c is the aerofoil chord. Given that, m = 0.045, q = 0.25, and using thinaerofoil theory estimate:i)The lift coefficient when the angle of attack (AOA) is given as 3°.ii) The zero-lift AOA of the aerofoil.iii) The moment coefficient with respect to the leading edge and the centre of pressurewhen the AOA is given as 3°.b) For an aerofoil similar to NACA 2412, the lift coefficient and moment coefficient aboutthe quarter-chord at -8° AOA are found to be -0.6 and -0.0466, respectively. At 6° AOA,these coefficients are found to be 0.86 and -0.0354, respectively.Giving reasons for your method, calculate the zero lift AOA and the location of theaerodynamic centre.

Step 1: Step 2: Step 3: Step 4:

Answered: Question 1 a) The mean camber line of…

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

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