# (Solved): Use following data of an aircraft at SLfor solving questions 4&5 : Wing Parameters Wing Paramet ...

Use following data of an aircraft at SLfor solving questions

4&5

: Wing Parameters

 Wing Parameters H. Tail Parameters AR =8,AR=5.5 \lambda =1.0,\lambda =1.0 S=18m^(2),S=3.5m^(2) V=5=0.

Other Parameters

AR=5.5

\lambda =1.0

S=3.5m^(2)

V=95(m)/(s)

x_(se)=0.25c

x_(cB)=0.3c

W=35000N

I_(2)=2000kg-m^(2)

\tau =0.5

i=2

deg

V=85(m)/(s)

(C_(m_(e)))_(frucluec )=-(0.005)/(r)ad

C_(L_(0))=0.31

i=-2deg

(C_(m_(Q)))_(twurches )=(0.10)/(r)adS_(D_(0))=0.03

C_(R_(Q))=-(0.005)/(r)adC_(L_(Se ))=(0.25)/(r)ad

C_(x_(u))=-0.17

C_(h_(se))=-(0.004)/(r)ad,L_(1)=5m

C_(L_(\alpha ))=(5)/(r)ad

C_(L_(a))=(4)/(r)ad

C_(z_(d))=-(2.6)/(r)ad

C_(m_(ac))=-0.12

C_(m_(ac))=0.0

C_(h_(0))=0

C_(Z_(4))=(7.5)/(r)ad

4. Calculate

C_(m_(l))

and

C_(m_(g))

contribution and Neutral point from above data for stick fixed and

(4,4,2)+

(3,3,2)

5. stick free case. 6. Calculate

x_(u),Z_(w),M_(a),M_(q)

and

M\alpha

. 2.5

5\times 1

(2,2)

We have an Answer from Expert