Chapter 6: stability and control
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=
0.42 (subsonic)
= 0.47 (supersonic)
Recall from Section 4.7 that
0.48. Since the F-16’s
is specified relative
to the leading edge of the
M.A.C.
it is convenient (and common)
to express
and
relative to the same reference. This requires subtracting the distance between
the root leading edge and the
M.A.C.
leading
edge from the value of
x
ac
.
The expression for
then becomes:
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left wing
longitudinal axis
= 0.47 (supersonic)
0.48. Since the F-16’s 
is specified relative 
and 
relative to the same reference. This requires subtracting the distance between