Id 112 - 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:
Question id 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)
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