Answer:
[tex]182.74020\ ^{\circ}C[/tex]
Explanation:
L = Initial length = 62.1 m
[tex]\alpha[/tex] = Coefficient of linear expansion of Aluminium = [tex]24\times 10^{-6}/^{\circ}[/tex]
[tex]T_i[/tex] = Initial temperature = 15°C
[tex]T_f[/tex] = Final temperature
[tex]\Delta L[/tex] = Change in length = 25 cm
Change in length due to heat is given by
[tex]\Delta L=L\alpha \Delta T\\\Rightarrow\Delta L=L\alpha (T_f-T_i)\\\Rightarrow T_f=\dfrac{\Delta L}{L\alpha}+T_i\\\Rightarrow T_f=\dfrac{0.25}{62.1\times 24\times 10^{-6}}+15\\\Rightarrow T_f=182.74020\ ^{\circ}C[/tex]
The temperature of the Concorde's skin in flight is [tex]182.74020\ ^{\circ}C[/tex]