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(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=2deg
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)ad4. 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)