A constant volume combustion gas turbine operates on
A.Ericsson cycle
B.Brayton cycle
C.Joule cycle
D.Atkinson cycle
A.Ericsson cycle
B.Brayton cycle
C.Joule cycle
D.Atkinson cycle
A.stagnation pressure to static pressure
B.isentropic work done to actual work
C.outlet whirl velocity to the blade velocity
D.none of the above
A.Reheating
B.Intercooling
C.Adding a regenerator
D.All of the above
E.None
A.an unsteady periodic and reversal of flow
B.the fixed mass flow rate regardless of pressure ratio
C.the reduction in lift force at higher angle of incidence
D.none of the above
A.greater the propulsive efficiency
B.Lesser the propulsive efficiency
C.unaffected is the propulsive efficiency
D.None of the above
A.no contamination of working substance with combustion gases
B.inferior quality fuel can be used
C.low maintenance costs
D.All of the above
A.Residual velocity loss
B.Leakage loss
C.Mechanical friction loss
D.Radiation loss
A.6 KSC
B.10 KSC
C.16 KSC
D.25 KSC
E.40 KSC
A.Reciprocating air compressor
B.Vane blower
C.Centrifugal blower
D.Axial flow compressors
A.Axial flow compressor
B.Sliding vane compressor
C.Centrifugal compressor
D.Lobe type compressor