Conduct a single cycle design points simulation for a turbojet engine in GasTurb
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Conduct a single cycle design points simulation for a turbojet engine in GasTurb

Question 1:

Conduct a single cycle design points simulation for a turbojet engine in GasTurb 13 with the below inputs and: 

a) Calculate the thrust specific fuel consumption. 

b) Calculate the Kinetic energy at Nozzle Exhaust. 

c) Plot h-s diagram for pressure ratio 15 and compare it with that of pressure ratio 18.8.


Hint
EngineeringH-S diagram: An H-S diagram is also k=called as the enthalpy–entropy chart and also known as the H–S chart or Mollier diagram. This diagram plots the total heat against entropy which describes the enthalpy of a thermodynamic system. Also, it's chart covers a pressure range of 0.01–1000 bar, and the temperatures up to 800 degrees Celsius....
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