ATPL: Given:- Ts the static temperature (SAT)- Tt the total temperature (TAT)- Kr the recovery coefficient- M the Mach numberThe total temperature can be expressed approximately by the formula:
Domanda 112, Aircraft General Knowledge - Instrumentation - ATPL - Airline Transport Pilot license
| Tt = Ts(1-0.2 M2) |
| Tt = Ts(1+0.2 M2) |
| Tt = Ts/(1+0.2 Kr.M2) |
| Tt = Ts(1+0.2 Kr.M2) |
