AviationTire Instrumentation Powerplant And System Monitoring Instruments Temperature Gauge Q 5 / 5

Given:

  1. M is the Mach number
  2. Ts is the static temperature
  3. Tt is the total temperature.

Ts = Tt.(1+0.2. M2)
Ts = Tt /(1+0.2. M2)
Ts = Tt.(0.2. M2)
Ts = Tt/( 0.2 M2)