10.8 An axial flow compressor with 50% degree of reaction is to have an overall com- pression ratio of seven. The inlet and exit blade angles are 50° and 15°, both mea- sured with respect to the axial...


10.8 An axial flow compressor with 50% degree of reaction is to have an overall com-<br>pression ratio of seven. The inlet and exit blade angles are 50° and 15°, both mea-<br>sured with respect to the axial direction. The inlet static temperature is 25°C and<br>the axial velocity can be assumed to be a constant at 160 m/s. If the isentropic<br>efficiency of the compressor is 0.88, estimate the stagnation temperature rise and<br>the number of stages required to achieve the desired compression ratio.<br>Ans: Aro=34.4°; Eight stages<br>

Extracted text: 10.8 An axial flow compressor with 50% degree of reaction is to have an overall com- pression ratio of seven. The inlet and exit blade angles are 50° and 15°, both mea- sured with respect to the axial direction. The inlet static temperature is 25°C and the axial velocity can be assumed to be a constant at 160 m/s. If the isentropic efficiency of the compressor is 0.88, estimate the stagnation temperature rise and the number of stages required to achieve the desired compression ratio. Ans: Aro=34.4°; Eight stages

Jun 11, 2022
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