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The inlet area of a gas turbine system is 0.06 m233i. Mass flow rate of the air through the turbine system . The air enters with a velocity of 110 m/s and has a specific volume of 0.85 m /kg. It exists at 145 m/s with a specific volume of 1.6 m /kg, determine ii. The exit area of the turbine system.

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The inlet area of a gas turbine system is 0.06 m233i. Mass flow rate of the air through the turbine system

. The air enters with a velocity of 110 m/s and has a specific volume of 0.85 m /kg. It exists at 145 m/s with a specific volume of 1.6 m /kg, determine

ii. The exit area of the turbine system.

 
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