In: Civil Engineering
1. The turbine of a hydrostatic plant is driven by a falling
head of water from a falling head of water from a source 30 m high
up through a 600 mm penstock flowing full.
A. Evaluate the theoretical velocity of water as it hits the
turbine blades in m/sec.
B. Evaluate the theoretical discharge of water in
m3/s.
C.If the turbine is only 70% efficient, estimate the horsepower
available from it..
2. Reservoir A supplies water to a nozzle having a diameter of
80 mm which is discharge water 40 m below the reservoir water level
at a velocity of 24m/s
A. Determine the loss of head in the pipeline.
B. Determine the horsepower produced by the jet.
C. Determine the efficiency of the nozzle.
3. The diameter of a pipe carrying water changes gradually from
150 mm at A to 450 mm at B. A is 5 m lower than B. If the pressure
at A is 70 kPa and at B is 50 kPa when 150 liters/ sec is
flowing.
A. Determine the direction of flow
B. Determine the frictional loss between two points
4. Reservoir A and B have elevations of 100 m and 160 m respectively. A pump is installed near reservoir A to pump the water from A to B. The rate flow in the pipe is 650 liters/sec. If the head loss in the pipeline is 8.22 m, compute the horsepower required to pump the water to B.
5. A reservoir A contains water at an elevation of 45 m and a 50 mm pipe line leads downhill from the reservoir and discharges into air at B at an elevation 0. If the loss of head between the reservoir A and B is 43.5 m compute the discharge flowing in the pipe.
6. A turbine is located at an elevation 200 m below that of the surface of the water at intake. the friction loss in the pipeline leading to it is 8 m and the turbine efficiency is 90%. What will be the power delivered by the turbine if the flow is 3 m3/ sec in kW?
7. Water is discharged through a nozzle having a diameter of jet
100 mm at a velocity of 60 m/s at a point 240 m below the
reservoir.
A. Compute the total headloss.
B. Compute the horsepower produced by the jet.
C. Compute the power lost in friction.
Ans 1-A) We know, theoratical velocity of water (V) =
where, H = Height of falling of water = 30 m
=> V =
=> V = 24.26 m/s
Ans 1-B) We know,
Flow rate (Q) = Area x velocity
Area of pipe = (/4)() = 0.2826 sq.m
=> Q = 0.2826 x 24.26
=> Q = 6.855 /s
Ans 1-C) We know,
Power delivered by turbine = g Q H
where, = water density = 1000 kg/m3
= efficiency = 70%
=> P = 1000 x 9.81 x 6.855 x 30 x 0.70
=> P = 1412198 W or 1893 hp
.
Ans 2-A) Apply Bernoulli between point 1 and 2 located at water surface elevation of reservoir and just outside nozzle respectively,
P1/ + /2g + Z1 = P2/ + /2g +Z2 + Hf
Since, both points are open to atmosphere, pressure is only atmospheric , hence gauge pressure P1 = P2 = 0
Velocity at surface is negligible so V1 =0
Elevation difference (Z1- Z2) = 40 m
Velocity at exit (V2) = 24 m/s
Hf is head loss due to friction
Putting values,
0 + 0 + 40 = 0 + /(2 x9.81) + Hf
=> 40 = 29.35 + Hf
=> Hf = 10.65 m
Hence, head loss in pipeline is 10.65 m
.
Ans 2-B) Horsepower produced by jet = g Q H / 746
Flow rate (Q) = Area x velocity
=> Q = (/4)() x 24 = 0.12 m3/s
=> Horsepower produced = 1000 x 9.81 x 0.12 x 40 / 746 = 63.12 hp
.
Ans 2-C) We know, nozzle efficiency = Actual discharge / Theoratical discharge
Theoratical discharge = area x theoratical velocity
=> Theoratical discharge= (/4)() x = 0.14 m3/s
=> Efficiency = 0.12 / 0.14
=> Efficiency = 0.857 or 85.7%