/sci/ - Science & Math

Anonymous Fri Apr 17 07:26:46 2020 No.11573986 [View]
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>>11565779
Can any anons help with this problem I am the big retard, got a question on Gas turbines where I am given T1 and P1 of air going from a compressor to a combustion chamber. the calorific value of the air fuel mixture within the CC. the CC outlet/turbine inlet temperature and pressure. the turbine outlet pressure. air fuel ratio, air feed rate. Cp for the compressor and turbine as well as their polytrophic indices. Given that I am told no dimension of inlets how am I supposed to calculate the mass flow rate of the fuel into the combustion chamber?

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/sci/ - Science & Math

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