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IDEAL TURBOFANENGINE
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Qnet
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Problem
Ambient Temperature= Ta =217K
Gamma=1.4
Cp=1.005 KJ/kg.K Qnet=42,800 KJ/kg
T04=1667K or 30000R
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Comparison
Turbofan performance VS c
Turbofan performance VS f
Turbofan performance VS
Turbofan performance VS Ma(Constant c & f)
Performance Parameters we are considering
Specific thrust
TSFC.
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increasing
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