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: | ATPL | ID: 112

Home > Examination quizzes for PPL(A), PPL(H), BPL Gas, BPL Hot Air, ATPL, SPL - Sailplane, EASA Drone > Quiz ATPL - Exam test Airline Transport Pilot license > Aircraft General Knowledge - Instrumentation > 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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