✈️
Density Altitude Calculator
Find density altitude from pressure altitude and temperature
📖 Density Altitude
Pilot-rule approximation: Density Altitude = Pressure Altitude + 118.8 × (T - Tₛₜd), with T in °C and Tₛₜd = 15 − 0.0019812 × Pressure Altitude(ft).
📊 Result
💡 Tips & Information
- High density altitude reduces aircraft performance.
- Pressure altitude can be read directly when altimeter is set to 29.92 inHg.
- Approximation valid within the troposphere and moderate temperature departures.