For efficient operation of axial flow compressors the blades are made
A.straight
B.slightly curved
C.aerofoil section
D.forward curved
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
A.an unsteady, periodic and reversal of flow in the compressor
B.the fixed mass flow rate regardless of pressure ratio
C.the reduction in lift force at higher angles of incidence
D.none of the above
A.reheating between expansion stage
B.intercooling between compression stges
C.regeneration
D.any of the above
A.decrease in net output as well as thermal efficiency
B.decrease in net output and increase in thermal efficiency
C.increase in net output but decrease in thermal efficiency
D.increase in net output as well as thermal efficiency
A.open cycle gas turbines only
B.closed cycle gas turbines only
C.both open as well as closed cycle gas turbines
D.none of the above
A.Screw compressor
B.Axial flow compressor
C.Roots blower
D.Vane blower
A.pressure ratio
B.compressor efficiency
C.turbine inlet temperature
D.All of the above
A.3000 rpm
B.1500 rpm
C.1000 rpm
D.375 rpm
E.50 rpm
A.Reciprocating type
B.Centrifugal type
C.Axial flow type
D.Lobe type
E.Sliding vane type