Table 6.3. Descriptive Parameters for an Early F-16A and an F-16C

Item	Early F-16A	F-16C
Wing:
S, ft2	300	300
croot, ft	16.5	16.5
ctip, ft	3.5	3.5
b, ft	30 (no missiles or rails)	30 (no missiles or rails)
x of root chord leading edge, ft	0 (20 ft aft of fuselage nose)	0 (20 ft aft of fuselage nose)
LE, degrees	40	40
Stabilator:
St, ft2	108	135
croot, ft	10	11
ctip, ft	2	3
b, ft	18	18
x of root chord leading edge, ft	17.5	17
LE, degrees	40	40
Strake (exposed)
Sstrake, ft2	20	20
croot, ft	9.6	9.6
ctip, ft	0	0
b, ft	2	2
x of root chord leading edge, ft	-8	-8
LE, degrees (avg.)	80	80
Fuselage
lf	48.5	48.5
wf	5	5
Whole Airplane
(relative to M.A.C.)	.35	.35

Adding the effect of the strake: