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TAS (True Airspeed)

Author: FLYTMExecutions: 31164
TOP/Shared Formulas (Science)/Physics (General)

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Calculates TAS (True Airspeed) based on IAS (Indicated Airspeed) [kt], ISA Deviation [°C], and altitude [ft].
IAS
kt
ISA Deviation
°C
Altitude
ft
TAS kt
Formula: IAS*171233*((288+ISAdev)-0.00198*ALT)^(0.5)/(288-0.00198*ALT)^2.628

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