i
PERFORMANCE, STABILITY, DYNAMICS, AND CONTROL
(CC,)c,=o=_[A+6 cA+osAct4)(:-, + ]
A +4 cos Ac/4
(CLct)e (CLcr)e
K=~:} a"==n_Ae aw2=~A
1.1CIA
e= R u .+ 1R)7rA
R = ai}~ + a217j + a3AI + a4
ai - 0.0004 a2 ~ -0.0080 a3 - 0.0501 a4 - 0.8642
We have
i. AA
Ai -
'I cos ALE
ao
CLr,e = ~+ _
Substituting ao - 0.1 *57.3 - 5.73/rad and A - 6, we get CUr,e = 0.0767/deg
or 4.3943/rad. With this, CL -. CIAr.ea - 0.3834. Further using Ac/4 = 0 and
A = 1.0, we get R - 0.9632, e - 0.9812, and K - 0.9942.
We have B = ~- = 1- Substituting, we get (CnplCL)C =O =
(Crip/CL)CL~.M = -0.6 and- (Cnp)W~ -0.2285. Therefore, the stnip theory
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