The ratio of inertia force to pressure forces is related with a non-dimensional number known as
A.Reyonolds number
B.Euler number
C.Nusselt number
D.Mach number
E.Weber number
A.Reyonolds number
B.Euler number
C.Nusselt number
D.Mach number
E.Weber number
A.0 – 4.5
B.100 – 140
C.100 – 200
D.200 – 300
E.300 – 800
A.Inertial forces to surface tension force
B.Intertial forces to viscous forces
C.Elastic forces to pressure forces
D.Viscous forces to gravity
E.Elastic forces to gravity
A.Inward projecting entrances
B.Fully rounded entrance having x/D>0.15
C.Gate in thin wall-unsuppressed contraction
D.Gate in thin wall-bottom and side suppressed
E.Gate in thin wall-corners rounded
A.Narrow sites
B.Wider sites
C.Small discharge
D.Low heads
E.Small discharge and low heads
A.144 lb/ft2
B.6.8046 x 10-2
C.6.8947 x 103 kg/m-sec2
D.0.06895 bar
E.Any of the above
A.Air drag
B.Friction in bearing
C.Direct current power for excitation
D.Heat generated in armature winding
E.All of the above
A.Inertial, viscous
B.Pressure, inertial, inetial
C.Gravity, pressure
D.Viscous, pressure
E.None of the above
A.Inward flow impulse turbine
B.Outward flow impulse turbine
C.Inward flow reaction turbine
D.Aoutward flow reaction turbine
E.Axial flow impulse turbine