In isentropic flow, the temperature
A.Cannot exceed the reservoir temperature
B.Cannot drop and then increase again downstream
C.Is independent of Mach number
D.Is a function of Mach number only
E.Remains constant in a duct flow
A.Cannot exceed the reservoir temperature
B.Cannot drop and then increase again downstream
C.Is independent of Mach number
D.Is a function of Mach number only
E.Remains constant in a duct flow
A.x4/5
B.x5/4
C.x3/5
D.x5/3
E.x1/2
A.Regardless of the motion of one fluid layer relative to an adjacent layer
B.When there is no motion of one fluid layer relative to an adjacent layer
C.Only when the fluid is frictionless
D.Only when fluid is frictionless and incompressible
E.Only when the fluid has zero viscosity and is at rest
A.Base power
B.Firm power
C.Primary power
D.Secondary power
E.Installed capacity
A.Is constant over the cross-section
B.Varies parabolically across the section
C.Is zero at the plates and linearly increases towards the plates
D.Is zero in the middle and increases linearly towards the plates
E.None of the above
A.Wet C.G.
B.Metacentre
C.Centre of pressure
D.Wet centre
E.Centre of buoyancy
A.Pressure
B.Velocity
C.Viscosity
D.Surface tension
E.Flow rate
A.4 – 5 m/s
B.10 – 12 m/s
C.12 – 12 m/s
D.20 m/s
E.25 m/s
A.In a liquid at rest
B.In a fluid at rest
C.In a laminar flow
D.In a turbulent flow
A.friction factor against Reynolds number
B.friction factor against log of Reynolds number
C.log of friction factor against Reynolds number
D.log of friction factor against log of Reynolds number