%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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Transcribed Image Text: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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