Aviation & Aeronautics
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Density Altitude

Pressure altitude corrected for temperature.

Formula

DA=PA+120(OATISA)DA = PA + 120(OAT - ISA)

Variables

PAPressure altitude
OATOutside temp
ISAStandard temp

Example

Hot air reduces performance

Did You Know?

On a hot day at a high airport, density altitude soars and aircraft struggle to generate lift.