Lt = L0*(1 + a*t) where a = coefficient of linear expansion and t = difference in temperature in °C to a first approximation. Lt = 30 - 0.05 = 29.95 and L0 = 30;
a = 23.1 x 10^-6
29.95/30 = 1 + 0.0000231*t
t = - 72 °C.
This temperature is relevant because at high altitudes, the temperature is low and around - 78 °C--I remember that I did see this on a Gulf Air flight.
Answers & Comments
Verified answer
An aluminum wing is 30 m long when its 20ºC.
At what temp. would the the wing be 5 cm shorter?
You have not provided enough information. You have to have some function that relates the
original length of the material, the expansion (or contraction) amount, and the temperature
difference. A constant of proportionality should a part of the function, as well. This constant
of proportionality is called the coefficient of linear expansion and is indicated by the Greek
letter α (alpha).
The general expansion formula can be expressed as:
e = αL∆t
Where:
e = expansion
L = original length
∆t = change in temperature
Given:
e = -5 cm = -0.05 m
α = 22.2 x 10^-6 (for aluminum)
L = 30 m
∆t = ?
We have to find the change in temperature in order to determine the temperature that will
cause the wing to shrink by 5 cm. Therefore, we have to rearrange the equation to make
∆t the unknown.
∆t = e/αL = -0.05/(22.2 x 10^-6)(30) = -75
∆t = -75°C
The temperature that will cause the wing to contract by 5 cm is
is given by 20°C - 75°C = -55°C
New t = -55°C
Lt = L0*(1 + a*t) where a = coefficient of linear expansion and t = difference in temperature in °C to a first approximation. Lt = 30 - 0.05 = 29.95 and L0 = 30;
a = 23.1 x 10^-6
29.95/30 = 1 + 0.0000231*t
t = - 72 °C.
This temperature is relevant because at high altitudes, the temperature is low and around - 78 °C--I remember that I did see this on a Gulf Air flight.