Engineering, 14.09.2019 03:30 zahrast14
Acentrifugal air (γ = 1.4) compressor raises the stagnation pressure from 93.3kpa at impeller inlet to 400kpa at diffuser outlet. the stagnation temperature at the compressor inlet is 293k. if the isentropic efficiency of the compressor is 0.8, calculate the stagnation temperature (in k) at the outlet of the diffuser. your answer must be rounded correctly to one decimal place. do not include the unit (k) in your answer.
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Acentrifugal air (γ = 1.4) compressor raises the stagnation pressure from 93.3kpa at impeller inlet...
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