Chapter 6: stability and control
phugoid longitudinal mode and the angle of attack oscillation is called the short period
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phugoid
longitudinal mode and the angle of attack
oscillation is called the
short period
mode. These oscillations are a consequence of the aircraft’s positive static stability.
Mean
Aerodynamic Chord
For
untapered wings
, the wing chord length is used
as the reference chord length
,
, in the expression for moment coefficient.
For tapered wings
, a simple average chord length is sometimes used. The
most commonly used value for
is known as the
mean
aerodynamic chord
(M.A.C.) The M.A.C. is a weighted average chord defined by the expression:
(6.11)
For untapered wings,
M.A.C.
=
c
.
For linearly tapered wings
, (6.11) simplifies to:
(6.12)
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left wing
longitudinal axis