True Airspeed Calculator

Posted by Dinesh on

This calculator calculates the true airspeed using indicated airspeed, mean sea level altitude, oat estimation correction values.

True Airspeed Calculation

Formula:

TAS = (IAS x OAT Estimation Correction) x (A / 1000) + IAS

Where,
IAS = Indicated Airspeed
A = Mean Sea Level (MSL) Altitude
TAS = True Airspeed