3.Air enters a gas turbine system with a velocity of 105 m/s and has a specific volume of0.8mkg. The inlet area of the gas turbine system is 0.05m. At exit the air has a velocity of135m/s and has a specific volume of L.5 m/kg. In its passage through the rurbine system thespecific enthalpy of the air is reduced by 145kj/kg and the air also has heat loss of 27kj kg.Determine7.1. The mass flow rate of the air through the turbine system2 The exit area of the turbine3. The power developed by the turbine systenm

Air inlet velocity, V1=105 m/s Specific volume of air at inlet, v1=0.8 m3/kg Inlet area of gas…

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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