Chapter 6: stability and control
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(6.8)
where
o
is the downwash angle when
= 0. This
is usually a very small angle
, often zero.
The
moment curve slope
,
, is obtained by taking the derivative of (6.7) with respect to absolute angle of attack:
(6.9)
(6.10)
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left wing
longitudinal axis
(6.8)
, is obtained by taking the derivative of (6.7) with respect to absolute angle of attack:
(6.9)
(6.10)