UNDERSTAND IT. WORK IT OUT.

Learn: Manning discharge

Manning’s equation estimates the discharge carried by an open channel under uniform-flow conditions. Roughness slows flow, while hydraulic radius and energy slope increase its carrying ability.

Beginner-friendlyFree · No accountTwo worked examples + separate practice
01

What the formula is saying

Calculate R^(2/3) and √S, multiply them, and divide by Manning roughness n. Finally multiply the mean velocity by flow area A to obtain discharge.

Q = (1/n) A R^(2/3) S^(1/2)

Read the symbols in plain language

n
Manning roughness

Empirical resistance coefficient for the stated channel surface. In this SI form its unit is s/m^(1/3); it is not a percentage.

s/m^(1/3)

Use s/m^(1/3) as the base unit shown here. Use the SI form: R in m, S as a dimensionless energy slope and n in s/m^(1/3). A is m² and discharge is m³/s. Hydraulic radius R = area/wetted perimeter is not generally water depth.

A
Flow area

Flow area. Multiply mean velocity by the wetted cross-sectional area.

m²

Square metres measure area; square the length conversion factor.

R
Hydraulic radius

Flow cross-sectional area divided by wetted perimeter. Do not include the open free surface in that perimeter.

m

Metres measure length; 1 m = 1000 mm.

S
Energy slope

Energy slope. Energy slope enters through its square root, using a decimal slope rather than whole percent.

ratio / no unit

A dimensionless ratio has no physical unit; 0.01 as a ratio is 1% when the percent option is selected.

Q
Result to find

Manning discharge. Multiply mean velocity by the wetted cross-sectional area.

m³/s

Sort out the units first

Use the SI form: R in m, S as a dimensionless energy slope and n in s/m^(1/3). A is m² and discharge is m³/s. Hydraulic radius R = area/wetted perimeter is not generally water depth.

Assumptions before calculating

Assume a prismatic reach with steady uniform free-surface flow and an appropriate roughness value. Energy slope equals bed slope only for the uniform-flow approximation; use S ≥ 0 as a magnitude.

02

Let’s solve one together

Read the given values, follow each operation, then check what the result means.

Read the supplied values as one complete study case. Find Q and explain the result in the stated output unit.

n · Manning roughness
0.013 s/m^(1/3)
A · Flow area
2 m²
R · Hydraulic radius
0.5 m
S · Energy slope
0.001
  1. Calculate the hydraulic-radius contribution

    The two-thirds power represents the geometric contribution in the Manning resistance model.

    (0.5)^(2 ÷ 3) ≈ 0.6299605249 m^(2/3)
  2. Take the square root of energy slope

    Energy slope enters through its square root, using a decimal slope rather than whole percent.

    √((0.001)) ≈ 0.0316227766
  3. Allow for channel roughness

    Dividing by the SI roughness coefficient gives the mean velocity for this reach.

    (0.6299605249) × (0.0316227766) ÷ (0.013) ≈ 1.532392381 m/s
  4. Convert velocity to discharge

    Multiply mean velocity by the wetted cross-sectional area.

    (2) × (1.532392381) ≈ 3.064784761 m³/s
Answer3.064784761 m³/s

Does this worked answer make sense?

Doubling n halves the result at unchanged geometry and slope. Multiplying S by four doubles it; multiplying S by two does not double it because the equation uses √S.

A second worked example — different values

A second case uses different data. Predict which way the answer will change, then calculate it without reusing the first answer.

n · Manning roughness
0.02 s/m^(1/3)
A · Flow area
3 m²
R · Hydraulic radius
0.7 m
S · Energy slope
0.002
  1. Calculate the hydraulic-radius contribution

    The two-thirds power represents the geometric contribution in the Manning resistance model.

    (0.7)^(2 ÷ 3) ≈ 0.7883735163 m^(2/3)
  2. Take the square root of energy slope

    Energy slope enters through its square root, using a decimal slope rather than whole percent.

    √((0.002)) = 0.04472135955
  3. Allow for channel roughness

    Dividing by the SI roughness coefficient gives the mean velocity for this reach.

    (0.7883735163) × (0.04472135955) ÷ (0.02) ≈ 1.762856774 m/s
  4. Convert velocity to discharge

    Multiply mean velocity by the wetted cross-sectional area.

    (3) × (1.762856774) ≈ 5.288570322 m³/s
Answer5.288570322 m³/s
03

Now try your own values

Change a value or its unit. The same method will show your calculation, step by step.

Empirical resistance coefficient for the stated channel surface. In this SI form its unit is s/m^(1/3); it is not a percentage.

Flow area. Multiply mean velocity by the wetted cross-sectional area.

Flow cross-sectional area divided by wetted perimeter. Do not include the open free surface in that perimeter.

Energy slope. Energy slope enters through its square root, using a decimal slope rather than whole percent.

English, Arabic and Persian digits are supported. The steps convert inputs to the formula’s base units.

Results update only when you calculate. The lesson example above stays unchanged.

04

Your turn — check your understanding

Solve this separate case yourself. Use only the values below; the two worked examples use different data. Give the requested result in the selected unit.

n · Manning roughness
0.015 s/m^(1/3)
A · Flow area
1.5 m²
R · Hydraulic radius
0.4 m
S · Energy slope
0.0015

Find: Learn: Manning discharge

For repeating decimals, use at least four significant figures. Accepted rounding tolerance: 0.05% of the expected value; zero uses an absolute tolerance of 10⁻¹².

A hint, not the answer

Calculate R^(2/3) and √S, multiply them, and divide by Manning roughness n. Finally multiply the mean velocity by flow area A to obtain discharge.

Use the SI form: R in m, S as a dimensionless energy slope and n in s/m^(1/3). A is m² and discharge is m³/s. Hydraulic radius R = area/wetted perimeter is not generally water depth.

Show the full practice solution

Compare the steps with your work; revealing a solution does not mark the lesson complete.

  1. Calculate the hydraulic-radius contribution

    The two-thirds power represents the geometric contribution in the Manning resistance model.

    (0.4)^(2 ÷ 3) ≈ 0.5428835233 m^(2/3)
  2. Take the square root of energy slope

    Energy slope enters through its square root, using a decimal slope rather than whole percent.

    √((0.0015)) ≈ 0.03872983346
  3. Allow for channel roughness

    Dividing by the SI roughness coefficient gives the mean velocity for this reach.

    (0.5428835233) × (0.03872983346) ÷ (0.015) ≈ 1.40171923 m/s
  4. Convert velocity to discharge

    Multiply mean velocity by the wetted cross-sectional area.

    (1.5) × (1.40171923) ≈ 2.102578845 m³/s
Answer2.102578845 m³/s

Avoid the common trap

Do not use ordinary pipe radius instead of hydraulic radius, put slope percent directly into S, or treat Manning n as a dimensionless percentage. A slope of 0.1% is 0.001.

When this method applies — and when it does not

This is an empirical resistance equation, not a complete gradually varied or rapidly varied flow analysis. Roughness depends on the channel, vegetation and flow stage. Do not import the US customary coefficient into this SI equation.

For study and understanding, not approval of a real structure, site operation or design. Apply the correct standard, National Annex and professional review to actual engineering work.

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Sources & further reading

References open in a new tab and explain the underlying principles. The teaching text and examples here are SimpleFlick’s own; the source organisations have not endorsed this calculator.

Reading focus: Manning discharge. Water-measurement principles; for discharge devices, read the orifice/weir chapters and the installation and head-measurement conditions, not only the coefficient formula.

Lesson updated: · Both examples and the separate practice case are checked against an independent high-precision numerical implementation. This verifies arithmetic for the stated model, not engineering certification.

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