Physics

Density Altitude Calculator

Find density altitude from pressure altitude and temperature.

Parameters Live Compute
Calculated Output
Density altitude 7,364.12
Formula: DA = PA + 118.8·(OAT − ISA)
Step-by-Step Breakdown
1. Values used:
2. Pressure altitude = 5,000
3. Outside air temperature = 25 °C
4.
5. Density altitude = 7,364.12
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Density altitude is the altitude the air 'feels like' to an aircraft — key for performance.

The math behind it

DA ≈ PA + 118.8·(OAT − ISA), where ISA temperature ≈ 15 − 1.98·(PA/1000) °C.

Worked Example

5000 ft pressure altitude at 25 °C → about 7375 ft density altitude.

Frequently Asked Questions

Why does hot weather hurt takeoff?

Higher density altitude means thinner air, reducing lift and engine power.

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