Air enters a gas turbine systenm with a velocity of 105 m/s and has a specific volume of 0.8m/kg. The inlet area of the gas turbine system is 0.05m2. At exit the air has a velocity of 135m's and has a specific volume of L.5 m/kg. In its passage through the turbine system the specific enthalpy of the air is reduced by 145kj/kg and the air also has heat loss of 27kj kg. Determine 1. The mass flow rate of the air through the turbine systeim 2 The exit area of the turbine 3. The power developed by the turbine system
Air enters a gas turbine systenm with a velocity of 105 m/s and has a specific volume of 0.8m/kg. The inlet area of the gas turbine system is 0.05m2. At exit the air has a velocity of 135m's and has a specific volume of L.5 m/kg. In its passage through the turbine system the specific enthalpy of the air is reduced by 145kj/kg and the air also has heat loss of 27kj kg. Determine 1. The mass flow rate of the air through the turbine systeim 2 The exit area of the turbine 3. The power developed by the turbine system
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
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Transcribed Image Text:3.
Air enters a gas turbine system with a velocity of 105 m/s and has a specific volume of
0.8mkg. The inlet area of the gas turbine system is 0.05m. At exit the air has a velocity of
135m/s and has a specific volume of L.5 m/kg. In its passage through the rurbine system the
specific enthalpy of the air is reduced by 145kj/kg and the air also has heat loss of 27kj kg.
Determine
7.
1. The mass flow rate of the air through the turbine system
2 The exit area of the turbine
3. The power developed by the turbine systenm
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