Aircraft Performance
Properties of the Atmosphere

The performance of any aircraft is highly dependent on the surrounding atmospheric properties. The following worksheet allows the atmospheric properties to be calculated, in particular density, pressure and temperature, up to an altitude of 50,000ft. The atmosphere equations are based on ISA definitions and are described in the chapter "Properties of the Atmosphere"

WorkSheet :   Properties of the Atmosphere

Application : International Standard Atmosphere Calculator 

Data Sheet : International Standard Atmosphere Tabulated Data

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