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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