Gas turbine used in aircraft is of
A.open cycle type
B.closed cycle type with reheating
C.closed cycle type with reheating and regeneration and intercooling
D.open cycle type with reheating, regeneration and intercooling
A.open cycle type
B.closed cycle type with reheating
C.closed cycle type with reheating and regeneration and intercooling
D.open cycle type with reheating, regeneration and intercooling
A.Sum of the forces is zero
B.Algebraic sum of the forces is zero
C.Sum of the resolved parts in any two perpendicular directions are both zero
D.None of the above
A.An instrument which indicates the condition of the battery
B.An instrument used for measurement of fuel consumption
C.An instrument for BHP measurement
D.An instrument for distance measurement
E.An instrument for smoke analysis
A.Single riveted butt joints
B.Double riveted butt joints
C.Single riveted lap joints
D.Double riveted lap joints
E.None of the above
A.Room temperature to 600?C
B.600?C to critical temperature
C.Between 800?C and 1200?C
D.Between 1400?C and 1530?C
E.None of the above
A.17,600 kg
B.12,540 kg
C.88 kg
D.4400 kg
E.2200 kg
A.at TDC and closes at BDC
B.10? before TDC and closes 10? after BDC
C.10? before TDC and closes 10? after BDC
D.10? before TDC and closes 50? after BDC
A.Halsey plan
B.Rowan plan
C.Emerson plan
D.none of the above
A.10 cubic metres of air
B.100 cubic metres of air
C.1000 cubic metres of air
D.10000 cubic metres of air
E.100000 cubic metres of air
A.Methane and ethane
B.Propane and butane
C.Petrol and diesel
D.Hexane and butadiene