Question
1. An axial flow compressor is required to deliver 50 kg/s of air at a stagnation pressure of 500 kPa. At inlet to the first
1. An axial flow compressor is required to deliver 50 kg/s of air at a stagnation pressure of 500 kPa. At
inlet to the first stage the stagnation pressure is 100 kPa and the stagnation temperature is 23C.
The hub and tip diameters at this location are 0.436 m and 0.728 m. At the mean radius, which
is constant through all stages of the compressor, the reaction is 0.50 and the absolute air angle
at stator exit is 28.8 for all stages. The speed of the rotor is 8000 rev/min. Determine the number
of similar stages needed, assuming that the polytropic efficiency is 0.89 and that the axial velocity
at the mean radius is constant through the stages and equal to 1.05 times the average axial velocity.
2. Derive an expression for the degree of reaction of an axial compressor stage in terms of the flow
angles relative to the rotor and the flow coefficient. Data obtained from early cascade tests suggested that the limit of efficient working of an axial-flow compressor stage occurred when
a relative Mach number of 0.7 on the rotor is reached;
the flow coefficient is 0.5;
the relative flow angle at rotor outlet is 30 measured from the axial direction;
the stage reaction is 50%.
Find the limiting stagnation temperature rise obtained in the first stage of an axial compressor
working under these conditions and compressing air at an inlet stagnation temperature of
289 K. Assume the axial velocity is constant across the stage.
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