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EAS201: Consider an ideal non-afterburning turbojet engine operating under the following conditions: Aerospace Propulsion Assignment, SUSS

Question 2
Consider an ideal non–afterburning turbojet engine operating under the following conditions:

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Taking into consideration the effects of fuel mass on engine thrust, evaluate the following:
Question 2a
Forward velocity in m/s.

Question 2b
Net thrust.

Question 2c
Specific thrust.

Question 2d
Output power of the engine.

Question 2e
Engine thermal efficiency.

Question 2f
Propulsive efficiency.

Question 2g
Thrust specific fuel consumption.

Question 2h
Exhaust exit Mach number.

Question 2i
Gas static temperature at exhaust exit.

Question 2j
Exhaust nozzle exit area.
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