Aerospace Engineering > GATE 2015 > Axial Turbines
Hot gas (ratio of specific heats, γ=1.33) at a temperature of 1450 K enters into an axial turbine and expands isentropically. Assume that the kinetic energy of the gas across the turbine is negligible. If the ratio of inlet to outlet pressures of the turbine is 9.5, then the temperature (in K) of gas exiting the turbine is
Correct : 824.0 to 832.1
Similar Questions
A single-stage axial turbine has a mean blade speed of 340 m/s at the design condition with blade angles at the inlet and exit of the rotor being 21° and 55° re...
If → denotes increasing order of intensity, then the meaning of the words dry → arid → parched is analogous to diet → fast → ______. Which one of the given opt...
If two positive non-zero real variables x and y are such that (x+y) is proportional to x/y, then x+y:
Total Unique Visitors
Loading......