| January 30, 2015

Combustion gases enter a gas turbine at 750°C and 1.2 MPa at a rate of 3.4 kg/s and leave at 630°C and 500 kPa. It is estimated that heat is lost from the turbine at a rate of


30 kW. Using air properties for the combustion gases and assuming the surroundings to be at 25°C and 100 kPa, determine (a) the actual and reversible power outputs of the turbine, (b) the exergy destroyed within the turbine, and (c) the second-law efficiency of the turbine.

Get a 5 % discount on an order above $ 150
Use the following coupon code :

Category: Coursework

Our Services:
Order a customized paper today!
Open chat
Hello, we are here to help with your assignments