accurate estimate of itsvalue is important to flight dynamics analysis. Since the side
force due torudder actswell behindthe cgit generates ayawing momentdescribed
as follows:
◦
N
ζ
ζ =−Yl
F
=−
1
2
ρV
2
S
F
l
F
a
2
R
ζ(13.201)
Thus, the simple expression for the dimensional derivative is ...
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