Home > Exam Quiz Archive > 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:

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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#### Explanation: 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:

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