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Densitetshoijdkalkylator

Berakna flygplanets prestationshojd

Pre-flightHot & high opsTakeoff performance

Density altitude decides whether your runway is long enough today.

The same paved strip that launched you yesterday might refuse you this afternoon. At 3,000 ft pressure altitude and 30°C, your indicated density altitude is closer to 5,500 ft — takeoff run can grow 30-50%, climb rate can halve.

Invarden

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Resultat

Lag paverkan

Tryckhojd

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Densitetshojd

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ISA-avvikelse

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grader C

Prestationsnotering

Normal flygplansprestanda forvantad

Om densitetshojd

Om densitetshojd Densitetshojd ar den hojd dar flygplanet "kanns" som om det flyger, baserat pa faktisk luftdensitet. Hogre densitetshojd innebar tunnare luft och reducerad flygplansprestanda.

Faktorer som okar densitetshojd: hog temperatur, lagt tryck, hog fuktighet, hog hojd.

ISA-avvikelse ISA-avvikelsen visar hur mycket den faktiska temperaturen skiljer sig fran International Standard Atmosphere-temperaturen pa given hojd (15C vid havsytan, minskar 2C per 1000ft).

Density Altitude (ISA Model)
DA = PA + (118.8 × (OAT − ISA_temp))
DA— Density altitude (feet)
PA— Pressure altitude (feet)
OAT— Outside air temperature (°C)
ISA_temp— ISA temperature at PA: 15 − 1.98 × (PA/1000)

How does density altitude affect your aircraft's performance?