Question: Air enters the diffuser of a turbojet engine with a mass flow rate (m) of 65 kg/s at 80 kPa, -40oC and a velocity of
Air enters the diffuser of a turbojet engine with a mass flow rate (m‹…) of 65 kg/s at 80 kPa, -40oC and a velocity of 245 m/s. The pressure ratio for the compressor is 10, and its isentropic efficiency is 87%. Air enters the turbine at 1000oC with the same pressure as the exit of the compressor. Air exits the nozzle at 80kPa. The turbine has an isentropic efficiency of 90%. Determine
(a) The rate of heat addition (Q‹…),
(b) The compressor power input (W‹… in) and
(c) The velocity of the air leaving the nozzle. Use the IG model.
(a) The rate of heat addition (Q‹…),
(b) The compressor power input (W‹… in) and
(c) The velocity of the air leaving the nozzle. Use the IG model.
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T, K T-S Plot from TEST using PG model It Turbojet Cycle5 1400.0 p=c 6 4 8 30 2 200.0 6.0 s, kuikg.K 8.0
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