
Christopher M. answered 05/03/23
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You need to know the metal's thermal expansion coefficient to solve this. Generally, you'll find this in a textbook or a handout. I looked it up online for plain aluminum and found 22.5 µm/(m ºC). I'll rewrite that as 22.5x10-6 m/(m ºC) to do the unit conversion right away and have everything in meters..
Thermal expansion or contraction is always a proportion of the original length, so
ΔL = αL0ΔT
Let's solve for ΔT to get
ΔT = ΔL/(αL0)
Now put in our given values. ΔL is negative since the wing shrank and a Δ is always final value - initial value
T-21°C = -0.06m/(22.5x10-6 m/(m ºC)×26m)
On the right, the meters all cancel leaving 1/(1/°C) which is just °C. That's a good sign! Having the right unit should give you confidence that the number along with it is also right.
T-21°C = -103°C
Solving for T gives us -82°C