The error in discharge (dQ/Q) to the error in measurement of head (dH/H) over a rectangular notch is given by dQ/Q = (3/2) × (dH/H) dQ/Q = (1/2) × (dH/H) dQ/Q = (dH/H) dQ/Q = (3/4) × (dH/H) TRUE ANSWER : ? YOUR ANSWER : ?
A Pelton wheel is Inward flow reaction turbine Tangential flow impulse turbine Inward flow impulse turbine Outward flow impulse turbine TRUE ANSWER : ? YOUR ANSWER : ?
Two dimensional flows occurs when The velocity of successive fluid particles, at any point, is the same at successive periods of time The magnitude and direction of the velocity do not change from point to point in the fluid The fluid particles move in plane or parallel planes and the streamline patterns are identical in each plane The direction and magnitude of the velocity at all points are identical TRUE ANSWER : ? YOUR ANSWER : ?
The efficiency of jet propulsion for a ship with inlet orifices at right angles to the direction of motion of ship is given by [2(Vr + v) v]/ Vr² [2(Vr - v) v]/ Vr² [(Vr + v) v]/ Vr [(Vr - v) v]/ Vr TRUE ANSWER : ? YOUR ANSWER : ?
The coefficient of discharge for an external mouthpiece is 0.5 0.855 0.707 0.375 TRUE ANSWER : ? YOUR ANSWER : ?
Braking jet in an impulse turbine is used None of these To change the direction of runner To break the jet of water To bring the runner to rest in a short time TRUE ANSWER : ? YOUR ANSWER : ?
The specific speed of a centrifugal pump, delivering 750 liters of water per second against a head of 15 meters at 725 r.p.m., is 24.8 r.p.m. 248 r.p.m 48.2 r.p.m 82.4 r.p.m. TRUE ANSWER : ? YOUR ANSWER : ?
The specific weight of water is 1000 kg/m” All listed here at mean sea level at normal pressure of 760 mm at 4°C temperature TRUE ANSWER : ? YOUR ANSWER : ?
Coefficient of resistance is the ratio of Actual velocity of jet at vena-contracta to the theoretical velocity Actual discharge through an orifice to the theoretical discharge Area of jet at vena-contracta to the area of orifice Loss of head in the orifice to the head of water available at the exit of the orifice TRUE ANSWER : ? YOUR ANSWER : ?
For hypersonic flow, the Mach number is greater than 4 greater than unity unity greater than 2 TRUE ANSWER : ? YOUR ANSWER : ?