Directly proportional to H1/2
Inversely proportional to H1/2
Directly proportional to H3/2
Inversely proportional to H3/2
C. Directly proportional to H3/2
At full load
At which there will be no damage to the runner
Corresponding to maximum overload permissible
At which the turbine will run freely without load
(1 + cos φ)/2
(1 - cos φ)/2
(1 + sin φ)/2
(1 - sin φ)/2
Waste valve closes suddenly
Supply pipe is long
Supply pipe is short
Ram chamber is large
0.25 m3/s
0.5 m3/s
1.5 m3/s
2.5 m3/s
Slow speed with radial flow at outlet
Medium speed with radial flow at outlet
High speed with radial flow at outlet
High speed with axial flow at outlet
To break the jet of water
To bring the runner to rest in a short time
To change the direction of runner
None of these
Velocity of flow at inlet to the theoretical jet velocity
Theoretical velocity of jet to the velocity of flow at inlet
Velocity of runner at inlet to the velocity of flow at inlet
None of the above
Low head of water
High head of water
Medium head of water
High discharge
Flow vs. swept volume
Pressure in cylinder vs. swept volume
Flow vs. speed
Pressure vs. speed
They have slow speeds
They are suitable even for low water heads
They give constant efficiency, even if the discharge is not constant
All of the above
Q/√H
Q/H
Q/H3/2
Q/H²
24.8 r.p.m.
48.2 r.p.m
82.4 r.p.m.
248 r.p.m
Directly as fan speed
Square of fan speed
Cube of fan speed
Square root of fan speed
In an impulse turbine, the water impinges on the buckets with pressure energy.
In a reaction turbine, the water glides over the moving vanes with kinetic energy.
In an impulse turbine, the pressure of the flowing water remains unchanged and is equal to atmospheric pressure.
In a reaction turbine, the pressure of the flowing water increases after gliding over the vanes.
Equal to
1.2 times
1.8 times
Double
10-15°
20-25°
30-40°
50-60°
Smoothen the flow
Reduce suction head
Increase delivery head
Reduce acceleration head
N/√H
N/H
N/H3/2
N/H²
(w Hm) / (Q × ηo)
(w Hm Q) / ηo
(w Q) / (Hm × ηo)
(w Q ηo) / Hm
At the level of tail race
Little above the tail race
Slightly below the tail race
About 2.5 m above the tail race to avoid cavitations.
Centrifugal pump
Reciprocating pump
Jet pump
Airlift pump
10 r.p.m.
20 r.p.m.
40 r.p.m.
80 r.p.m.
Ratio of actual discharge to the theoretical discharge
Sum of actual discharge and the theoretical discharge
Difference of theoretical discharge and the actual discharge
Product of theoretical discharge and the actual discharge
Screw pump
Gear pump
Cam and piston pump
Plunger pump
4
6
8
12
An axial flow
An inward flow
An outward flow
A mixed flow
Directly as fan speed
Square of fan speed
Cube of fan speed
Square root of fan speed
Net head
Absolute velocity
Blade velocity
Flow
P/ √H
P/ H
P/ H3/2
P/ H²
Directly proportional to N
Inversely proportional to N
Directly proportional to N²
Inversely proportional to N²