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Consider a radial turbine receiving air at 800deg C with an outer rotor radius r_(2)=0.05m . The pressure ratio across the turbine stage is ((P_(01))/(P_(03)))=2.1
Consider a radial turbine receiving air at
800\\\\deg C
with an outer rotor radius
r_(2)=0.05m
. The pressure ratio across the turbine stage is
((P_(01))/(P_(03)))=2.1
and the isentropic efficiency is
89%
. Calculate the required rotating speed of the rotor
(rpm)
. Take
C_(p)=1.15k(J)/(k)gK
and
\\\\gamma =1.33
. Consider no swirl at exit of the turbine.
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