The efficiency of a jet propulsion unit is generally high at altitudes of
A.1000 metres
B.5000 metres
C.7500 metres
D.9000 metres
E.More than 10,000 metres
A.1000 metres
B.5000 metres
C.7500 metres
D.9000 metres
E.More than 10,000 metres
A.Toluene
B.Benzene
C.Isoctave
D.n-heptane
E.Alcohol
A.2.327 ata
B.1.2 ata
C.1.127 ata
D.0.563 ata
E.0.073 ata
A.1 mm Hg
B.13.6 cm of water column
C.760 mm of water
D.760 mm of Hg
E.None of the above
A.To improve thermal efficiency
B.To clean the surfaces by carrying away the carbon and metal particles cansed by wear
C.To reduce noise
D.To reduce vibrations
E.None of the above
A.Created at the beginning of suction stroke
B.Created at the end of suction stroke
C.Created during combustion
D.Created towards the end of compression stroke
E.None of the above
A.Not running
B.Running
C.During starting
D.During cranking
E.None of the above
A.1
B.0.528
C.0.546
D.0.577
E.0.75
A.Upto 100?C
B.100 – 250?C
C.250 – 500?C
D.Above 500?C
E.Below 100?C
A.The sum of internal energy and the work done in forcing unit mass of substance into an enclosure at the constant pressure at which the substance exists
B.Sum of sensible heat + latent heat of substance
C.Total heat content of substance above zero degree centigrade
D.Sensible heat of water + work done in forcing unit mass of substance into an enclosure at constant pressure at which the substance exists
E.None of the above