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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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