William W. answered 07/17/22
Experienced Tutor and Retired Engineer
Let's assume the aircraft wing is composed largely of aluminum 7075. The coefficient of thermal expansion for Al 7075 is 23.6 µm/m-°C.
If we convert 7 cm into µm, we get 70,000 µm. so:
(70,000/37)/23.6 = 80.16 °C
Since we start at 23 °C and the wing is getting colder, then subtracting 80 would get us to -57 °C