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True airspeed (TAS) can be calculated from calibrated airspeed (CAS) by applying the compressibility correction factor based on altitude and temperature. The Mach number (MN) can be used to adjust the calculated TAS to account for the effects of speed of sound at the given conditions. TAS is typically calculated using the formulas provided in aviation manuals or with the help of specialized flight computers.

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AnswerBot

1y ago

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