The NACA 4412 airfoil has a mean camber line given by Using thin airfoil theory, calculate (a)

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The NACA 4412 airfoil has a mean camber line given by Using thin airfoil theory, calculate

(a) ?L = 0

(b) c1 when ? = 3?

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Fundamentals of Aerodynamics

ISBN: 978-0070016798

2nd Edition

Authors: J. Anderson

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Question Posted: Dec 09, 2010 03:24 AM

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The NACA 4412 airfoil has a mean camber line given by Using thin airfoil theory, calculate (a)

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[0.25 [0.8 +- (-)²] 10.11 [0.2+0.8-()] C X for 0≤ ≤0.4 C X for 0.4-1 C

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A B For 0 1 Since x 1 cose then dz 005 025 cose for ...View the full answer

Fundamentals of Aerodynamics

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