Formula:

w = K / ((K - 1) * R * T₁ * [1 - ((p₂ / p₁)^((K-1)/K))])


Where,
w = Specific Work Gas Turbine
K = Ratio Specific Heat Air
R = Individual Gas Constant
T₁ = Absolute Temperature
p₁ = Primary Pressure
p₂ = Secondary Pressure

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