The NACA 4412 airfoil has a mean chamber line given by0.25for 0ss0.4l0.111 02+ 08: - ()'|0.111 0.2 + 0.8 – (4)*|for 0.4 ss1Using thin airfoil theory, calculate Cme/4 and Xcp/C when a =3°%3DNIU

a Let 0≤xc≤0.4; dtdx1=0.2-0.5xc 0.4≤xc≤1; dtdx2=0.0888-0.2222xcsince…

Answered: %3D irfoil has a mean chami (0.25…

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%3D irfoil has a mean chami (0.25 (08²-()

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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Question

The NACA 4412 airfoil has a mean chamber line given by
0.25
for 0ss0.4
l0.111 02+ 08: - ()'|
0.111 0.2 + 0.8 – (4)*|
for 0.4 ss1
Using thin airfoil theory, calculate Cme/4 and Xcp/C when a =3°
%3D
NIU

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