The moment coefficient with respect to the leading edge and the centre of pressure when the AOA is given as 4º.
The moment coefficient with respect to the leading edge and the centre of pressure when the AOA is given as 4º.
Advanced Engineering Mathematics
10th Edition
ISBN:9780470458365
Author:Erwin Kreyszig
Publisher:Erwin Kreyszig
Chapter2: Second-order Linear Odes
Section: Chapter Questions
Problem 1RQ
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Question
Transcribed Image Text:a) The mean camber line of an aerofoil is defined by the relations:
X X
17²7 ( 29 - *) * 2 * ²
2
q
с C с
Zc m
C
Zc
C
m
(1-q)²
≤q,
X
(1-9)²-( \ / -9
9
C
Given that, c is the aerofoil chord, m = 0.025, q = 0.45, and using thin aerofoil theory
estimate:
Transcribed Image Text:iii)
The moment coefficient with respect to the leading edge and the centre of
pressure when the AOA is given as 4º.
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