Hydropower: Resources, Plant Layout, Head and Flow, Pelton, Francis and Kaplan Turbines, Small Hydro
2. Plant layout and penstock losses
Along the water path come: the dam or weir that raises the level and stores or diverts water; the intake with a trash rack to stop debris; a canal or tunnel (a forebay where the water joins the penstock); the penstock, the steep pressure pipe to the turbine; a surge tank that absorbs pressure surges when the flow is changed suddenly (water hammer) on long conduits; the powerhouse with turbine, governor and generator; and the draft tube (reaction turbines) and tailrace returning the water. Isolating valves and spillways protect the structure in floods.
Friction in the penstock reduces the net head. By the Darcy-Weisbach relation hf = f L v²/(2gD), with v = Q/(πD²/4). Worked example. L = 500 m, D = 1.5 m, Q = 6 m³/s, friction factor f = 0.02 (given): v = 6/1.767 = 3.395 m/s; hf = 0.02 × 500 × 3.395²/(2 × 9.81 × 1.5) = 3.92 m. Because hf grows as Q², there is a best flow for a given pipe: the power ρgQ(Hg − kQ²) is largest when hf = Hg/3, so the net head at the maximum is 2Hg/3. A designer uses a larger pipe to keep hf to a few percent of Hg, since the pipe is a major cost.
3. Pelton, Francis and Kaplan turbines
| Turbine | Action and flow | Head and flow | Features |
|---|---|---|---|
| Pelton | impulse; free jets strike split buckets at atmospheric pressure; tangential | high head, small flow | regulated by a spear valve and jet deflector; no draft tube |
| Francis | reaction; pressure falls across the runner; radial inflow, mixed outflow | medium head, medium flow | guide vanes regulate; draft tube; most widely used |
| Kaplan | reaction; axial flow; adjustable runner blades | low head, large flow | keeps good efficiency at part load by adjusting the blade angle with the guide vanes; draft tube |
Selection by specific speed. The specific speed Ns = N√P/H^(5/4), with N in rpm, P in kW (the shaft power) and H in m, is the speed of a geometrically similar turbine that gives 1 kW under 1 m of head; it collects speed, power and head into one number that describes the shape of the runner. Typical ranges (metric units, indicative): Pelton about 10 to 60 (single jet at the lower end), Francis about 60 to 300, Kaplan about 300 to 1000. Low Ns means a high-head, small-flow machine, and high Ns a low-head, large-flow one. Worked example. N = 300 rpm, P = 10 000 kW, H = 100 m: Ns = 300 × 100/100^1.25 = 30 000/316.2 = 94.9, in the Francis range.
Pelton basics. The jet speed is V₁ = Cv√(2gH), with Cv ≈ 0.98 for the nozzle. The best bucket speed u is a little under V₁/2, for example 0.46V₁ in practice; for a frictionless 180° deflection, u = V₁/2 gives the whole kinetic power of the jet: P = ρQ u (V₁ − u)(1 + 1). With Q = 0.15 m³/s, V₁ = 80 m/s and u = 40 m/s, P = 1000 × 0.15 × 40 × 40 × 2 = 480 kW, equal to ½ρQV₁² = 480 kW. A real bucket turns the jet by less than 180° and has friction, so the power is less. Wheel speed: with H = 400 m, Cv = 0.98, u = 0.46V₁ and wheel diameter 1.4 m, V₁ = 86.8 m/s, u = 39.9 m/s and N = 60u/(πD) = 545 rpm.
4. Draft tube, cavitation and part-load behaviour
Draft tube and cavitation. The draft tube of a reaction turbine is a diverging passage that recovers the exit kinetic energy and lets the runner sit above the tailwater, using the suction head. Setting the runner too high drops the local pressure towards the vapour pressure and causes cavitation, which pits blades and loses efficiency. The Thoma coefficient σ = (Ha − Hv − Hs)/H, with Ha the atmospheric head, Hv the vapour-pressure head and Hs the setting above the tailwater, must exceed the critical value for the turbine; a larger Hs lowers σ and invites cavitation. Pelton runners run in air and do not cavitate in this way.
Part-load behaviour. Demand and flow change, so the efficiency-against-load curve matters. A Pelton wheel with a spear valve, especially a multi-jet one, and a double-regulated Kaplan turbine keep a high efficiency over a wide range of load. A Francis turbine, with fixed runner blades, falls off noticeably at part load, and a fixed-blade propeller turbine falls sharply. The overall efficiency is the product of the hydraulic, mechanical (bearing) and generator efficiencies, η = ηh ηm ηg; for example 0.92 × 0.98 × 0.97 = 0.875, so about one-eighth of the water power is lost even at best.
5. Small hydro systems
Small hydro is hydropower at a modest scale, generally run-of-river with a diversion weir and a short penstock and no large reservoir, so it has far less submergence and a smaller environmental footprint than a large dam. The size limit for “small” differs between countries, so classes are best remembered by name in descending order: small, mini, micro and pico. Equipment is standardised and often built locally; plants are placed on canals, drops in irrigation channels and mountain streams.
- Turbine choice follows head and flow: Pelton or Turgo for high head and small flow; Francis for medium head; Kaplan, propeller or tubular types for low head; the cross-flow (Banki) turbine is simple, cheap, tolerant of changing flow and common in micro hydro at low to medium head.
- Design flow is picked from the flow-duration curve: a higher design flow gives more energy but a larger, costlier turbine that runs part-loaded on more days.
- Generators and control: small plants often use induction or synchronous generators; an isolated micro-hydro plant with a fixed-speed generator holds frequency with an electronic load controller that diverts surplus power to a ballast (dump) load, instead of a costly mechanical governor.
Key takeaways
- P = ηρgQH with the net head H = Hg − hf; hf = fLv²/(2gD), and for a fixed pipe the maximum power occurs when hf = Hg/3.
- The flow-duration curve shows time for which flow is equalled or exceeded; design flow and energy come from it. Run-of-river follows the river; storage follows demand; pumped storage stores energy.
- Pelton: impulse, high head, free jets at atmospheric pressure, spear valve. Francis: reaction, medium head, guide vanes. Kaplan: axial, low head, adjustable blades, good part-load efficiency.
- Ns = N√P/H^(5/4) (rpm, kW, m): low for Pelton, medium for Francis, high for Kaplan. Pelton jet V₁ = Cv√(2gH) and bucket speed near 0.45V₁; ideal 180° deflection gives all the jet power at u = V₁/2.
- A draft tube recovers exit kinetic energy but a high setting risks cavitation (Thoma σ = (Ha − Hv − Hs)/H). Small hydro is run-of-river; cross-flow, Pelton, Kaplan-type machines suit it by head, and micro plants use a load controller.
Practice questions (18)
Attempt each one before opening the answer. Every explanation names the tempting wrong option as well as the right one, because that is where marks are lost.
A site has a very high head of several hundred metres and a small flow of water. Which turbine suits it best?
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Answer: B — Pelton wheel
A high head with small flow gives a low specific speed, which is the Pelton range. Kaplan and propeller machines are for low head with large flow.Which turbine has an axial flow runner with adjustable blades and is used for low heads?
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Answer: D — Kaplan turbine
The Kaplan turbine has axial flow and runner blades whose pitch can be adjusted with the guide vanes. The Francis has fixed runner blades and radial inflow, and Pelton and Turgo are impulse machines for high head.Which statement distinguishes an impulse turbine such as the Pelton wheel from a reaction turbine such as the Francis?
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Answer: A — In the Pelton wheel the whole pressure drop occurs in the nozzle, and the jet strikes the buckets at atmospheric pressure
In an impulse turbine the head is converted to jet velocity in the nozzle and the buckets only change its direction at atmospheric pressure. In a reaction machine the runner passage is full and the pressure drops across it.A turbine has N = 300 rpm, delivers P = 10 000 kW at a net head H = 100 m, and specific speed Ns = N√P/H^(5/4). If specific speed ranges of about 10 to 60 (Pelton), 60 to 300 (Francis) and 300 to 1000 (Kaplan) are taken, the suitable turbine is
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Answer: C — Francis turbine, since Ns is about 95
Ns = 300 × √10 000/100^1.25 = 300 × 100/316.2 = 94.9, within the Francis range. The Kaplan answer would follow if H were mistakenly dropped from the denominator.What is the main function of the draft tube of a reaction turbine?
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Answer: D — It recovers exit kinetic energy and lets the runner sit above the tailwater
The diverging draft tube slows the water, converting velocity head into pressure recovery, and uses the suction head below the runner. Surge absorption is the job of a surge tank, and regulation of flow is done by the guide vanes.A Francis turbine runner is moved higher above the tailwater level, with head and flow unchanged. What is the main risk?
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Answer: A — Cavitation, because the Thoma coefficient falls and the outlet pressure nears the vapour pressure
σ = (Ha − Hv − Hs)/H falls as Hs grows, and the lower pressure at the outlet drops toward the vapour pressure, so cavitation sets in. Setting height does not alter the specific speed formula and has no effect on penstock friction.A penstock of fixed size feeds a turbine from a reservoir of fixed gross head Hg, and friction loss is proportional to Q². The flow that gives the maximum power is the one at which the friction head loss is
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Answer: C — Hg/3
P ∝ Q(Hg − kQ²); setting dP/dQ = 0 gives Hg = 3kQ², so hf = kQ² = Hg/3. At hf = Hg the net head is zero and so is the power.The purpose of a surge tank on a long penstock is to
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Answer: B — absorb the pressure surges caused by sudden changes in flow (water hammer)
A surge tank gives a free surface that lets the water column move and limits the pressure rise when the turbine gates close quickly. Debris is stopped by the trash rack and seasonal storage is the job of the reservoir.A micro-hydro scheme on a small stream has a low-to-medium head, wide variations of flow, and needs a simple, cheap turbine that is easily made locally. Which turbine is the most natural choice?
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Answer: A — A cross-flow (Banki) turbine
The cross-flow turbine is simple, tolerates variable flow with good part-load efficiency, and is widely used in micro hydro. A Francis or double-regulated Kaplan is costly and complex, and a Pelton is for high head.Which statement about a flow-duration curve of a river is correct?
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Answer: D — It plots the flow against the fraction of time for which that flow is equalled or exceeded, and the area under it gives the available volume of water
Ordering the flows from largest to smallest against the exceedance fraction gives the curve, and its area is the volume per year. A chronological plot is a hydrograph, not a duration curve.Which of the following statements about the Pelton wheel are correct?
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Answer: A — It is an impulse turbine; B — The jet strikes the buckets at atmospheric pressure; C — The flow is regulated by a spear valve in the nozzle
The impulse action, the atmospheric-pressure jet and the spear-valve regulation are standard properties of the Pelton wheel. The wheel runs in air above the tailwater, so it has no draft tube.Which of the following statements about reaction turbines are correct?
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Answer: A — Francis and Kaplan turbines are fitted with a draft tube; B — A Kaplan turbine keeps good efficiency at part load by adjusting its runner blade angle; D — The specific speed of a Francis turbine is higher than that of a Pelton wheel
Both reaction machines use a draft tube, the Kaplan is double-regulated with adjustable runner blades, and Ns rises from Pelton to Francis to Kaplan. A Kaplan with fixed blades would be a propeller turbine.Which of the following statements about hydropower schemes are correct?
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Answer: A — The output of a hydro plant is proportional to the product of flow and net head; B — A small run-of-river plant has little storage and its output follows the river flow; D — The design flow of a plant is chosen with the help of the flow-duration curve
P = ηρgQH, run-of-river output follows the river, and the flow-duration curve fixes the design flow. Load varies in a micro-hydro plant, so a load controller or governor is needed to hold the frequency.A hydro plant has a flow of 20 m³/s, a gross head of 100 m and a head loss of 5 m in the waterway. The overall efficiency is 0.88, water density 1000 kg/m³ and g = 9.81 m/s². The electrical power output in MW, to one decimal place, is ____.
Numerical answer — type the value.
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Answer: 16.4
Net head = 100 − 5 = 95 m; P = 0.88 × 1000 × 9.81 × 20 × 95 = 16.40 × 10⁶ W = 16.4 MW. Using 100 m gives 17.3 MW. Verified in Python (16.402).A penstock of length 500 m and diameter 1.5 m carries 6 m³/s of water. Using the Darcy-Weisbach equation hf = fLv²/(2gD) with friction factor f = 0.02 and g = 9.81 m/s², the head loss in metres, to two decimal places, is ____.
Numerical answer — type the value.
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Answer: 3.92
v = Q/(πD²/4) = 6/1.7671 = 3.3953 m/s; hf = 0.02 × 500 × 3.3953²/(2 × 9.81 × 1.5) = 115.28/29.43 = 3.917, i.e. 3.92 m. Verified in Python.A turbine runs at N = 300 rpm, delivers P = 10 000 kW (shaft power) under a net head H = 100 m. Its specific speed Ns = N√P/H^(5/4) (rpm, kW, m), rounded to the nearest whole number, is ____.
Numerical answer — type the value.
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Answer: 95
Ns = 300 × √10 000/100^1.25 = 300 × 100/316.23 = 94.87, i.e. 95. Verified in Python.A Pelton wheel works under a net head of 400 m. The nozzle coefficient is Cv = 0.98, so the jet speed is V₁ = Cv√(2gH) with g = 9.81 m/s². The bucket speed is 0.46V₁ and the wheel (pitch-circle) diameter is 1.4 m. The wheel speed in rpm, rounded to the nearest whole number, is ____.
Numerical answer — type the value.
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Answer: 545
V₁ = 0.98 × √(2 × 9.81 × 400) = 0.98 × 88.59 = 86.82 m/s; u = 0.46 × 86.82 = 39.94 m/s; N = 60u/(πD) = 60 × 39.94/(π × 1.4) = 544.8, i.e. 545 rpm. Verified in Python.A frictionless Pelton bucket deflects the jet through 180°. The jet speed is 80 m/s, the jet discharge is 0.15 m³/s, water density is 1000 kg/m³, and the bucket speed is 40 m/s. Using P = ρQ u (V₁ − u)(1 + cos 0°), the power developed, in kW, is ____.
Numerical answer — type the value.
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Answer: 480
P = 1000 × 0.15 × 40 × (80 − 40) × (1 + 1) = 1000 × 0.15 × 40 × 40 × 2 = 480 000 W = 480 kW, which equals the jet kinetic power ½ρQV₁² = 0.5 × 1000 × 0.15 × 6400 = 480 kW, so the ideal efficiency is 100 %.