T1 is the initial temperature and T is the final temperature. B is a linear temperature expansion coefficient. dt - the change of the temperature. l -- length of aluminum wing.
B=l1×dtdl
dt=l1×Bdl
l1=0.025 [m1]dl=−0.06 [m]
dt=0.025×22.2×10−60.06=10−66.7×10−5=−67 oC
T=T1+dt=(19−67) oC=−48 oC
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