Air at a temperature of 350 K enters a centrifugal compressor running at 16000 rpm, The impeller diameter is 0.6 m and isentropic efficincy of compressor is 0.88. Assume that absolute velocities at inlet and outlet are equal. If the slip factor and work factor are 0.9 and 1.05 respectively; pressure ratio developed is
Impeller diameter, D2=0.6m
N=16000rpm
u2=πD2N60=π×0.6×1600060=502.654 m/s
Slip factor,ϕs=0.9
Work factor,ϕw=1.05
Inlet factor,T1=350 K
As we know, compressor work ,
ωc=cp(T2−T1)=ϕsϕwu22
⇒1.005×1000(T2−350)=0.9×1.05×502.6542
T2=587.577 K
ηc=0.88=T2s−T1T2−T1=T2s−350587.577−350
⇒T2s=559.068 K
T2sT1=rγ−1p/γ
559.068350=(rp)1.4−1/1.4
Pressure ratio,rp=5.15