(a) Lost work
(d) Loss of stage efficiency due to cooling
Cª heat rejected/stage work
(e) Small stage efficiency
B.(a) Draw a sketch of the two-stage axial flow compressor with inlet guide vanes.
(b) Draw curves indicating the variation of static pressure, temperature and absolute velocity through this compressor.
(c) Why does a compressor stage have a lower efficiency and loading factor compared to an equivalent turbine stage?
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