Thermal efficiency of a gas turbine is in the range
A.50 to 60 percent
B.40 to 50 percent
C.30 to 40 percent
D.20 to 30 percent
A.50 to 60 percent
B.40 to 50 percent
C.30 to 40 percent
D.20 to 30 percent
A.reheat the steam
B.increase the specific output
C.reduce exhaust pressure
D.reduce work done
A.Roots blower
B.Centrifugal compressor
C.Axial flow compressor
D.All of the above
A.Otto cycle is more efficient
B.Brayton cycle is less efficient
C.Brayton cycle is for slow speed engines only
D.Large volume of low pressure gas cannot be efficiently handled in reciprocating engines
A.unequal
B.equal
C.not related to each other
D.none of the above
A.It is bulky in size
B.cooling arrangement does not exist
C.operating speeds are too high
D.it is driven by an electric motor
A.subsonic
B.sonic
C.supersonic
D.supersonic on one side and subsonic on the other side
A.limits of compressor discharge
B.limit of compressor efficiency
C.limit of stable operation
D.lower critical speed of shaft
A.straight
B.slightly curved
C.aerofoil section
D.forward curved
A.Open cycle gas turbine with regeneration
B.Open cycle gas turbine with intercooling
C.Open cycle gas turbine with reheating and regeneration
D.Closed cycle gas turbine