The atmosphere becomes colder at higher elevation. As an average the standard atmospheric absolute temperature can be expressed as Tatm = 518 - 3.84 × 10−3 z, where z is the elevation in feet. How cold is it outside an airplane cruising at 32000 ft expressed in Rankine and in Fahrenheit?
For an elevation of z = 32 000 ft we get
Tatm = 518 – 3.84 × 10−3 z
= 395.1 R
To express that in degrees Fahrenheit we get
TF = T – 459.67 = −64.55 F