---
title: "Continuity in cylindrical coordinates, radial flow"
subject: "Fluid Mechanics"
chapter: 4
key: "semester_4/fluid_mechanics_mechanical:continuity-cylindrical-radial-flow"
source: https://www.bctengineer.com/q/semester_4/fluid_mechanics_mechanical/continuity-cylindrical-radial-flow
site: BCT Engineering
---

# Continuity in cylindrical coordinates, radial flow

Fluid Mechanics · Chapter 4: Basic Equations for Fluid Flow

- Asked in: year not given, 3+3 marks
- Video: [Derivation of the Continuity Equation in Cylindrical Coordinates](https://www.youtube.com/watch?v=95jHgmcLzoM) — Fluid Matters
- Answer checked by Claude Opus 5.5 (high effort) on 2026-10-14
- Page: https://www.bctengineer.com/q/semester_4/fluid_mechanics_mechanical/continuity-cylindrical-radial-flow
- Whole chapter: https://www.bctengineer.com/md/semester_4/fluid_mechanics_mechanical/chapter-4

## Question

(a) Write the continuity equation for steady incompressible flow in cylindrical coordinates $(r, \theta, z)$ and explain each term.
(b) Water enters at the centre of two parallel circular discs 20 mm apart and flows radially outward. The discharge is 0.04 m$^3$/s. Show that the flow satisfies continuity and find the radial velocity at radii 0.10 m and 0.25 m.

## Short answer

The steady incompressible continuity equation in cylindrical coordinates is (1/r)∂(rv_r)/∂r + (1/r)∂v_θ/∂θ + ∂v_z/∂z = 0. For radial flow between parallel discs, v_r = Q/(2πrb). With Q=0.04 m³/s and b=0.02 m, v_r = 3.18 m/s at r=0.10 m and 1.27 m/s at r=0.25 m.

## Answer

#### (a) Continuity equation in cylindrical coordinates
With velocity components $v_r$ (radial), $v_\theta$ (tangential) and $v_z$ (axial):

$$
\frac{1}{r}\frac{\partial (r v_r)}{\partial r} + \frac{1}{r}\frac{\partial v_\theta}{\partial \theta} + \frac{\partial v_z}{\partial z} = 0
$$

- First term: net radial outflow per unit volume. The factor $r$ appears because the flow area $r\,d\theta\,dz$ grows with $r$.
- Second term: net tangential outflow per unit volume. The factor $1/r$ appears because the arc length of the element is $r\,d\theta$.
- Third term: net axial outflow, the same as in the Cartesian form.

For compressible unsteady flow the term $\partial\rho/\partial t$ is added and $\rho$ is included inside the derivatives. For axisymmetric flow, $\partial/\partial\theta = 0$.

#### (b) Radial flow between discs
Given $b = 0.02\ \text{m}$, $Q = 0.04\ \text{m}^3/\text{s}$. The flow is radial and symmetric, so $v_\theta = 0$, $v_z = 0$, and the flow area at radius $r$ is $2\pi r b$.

From continuity (a volume balance), $v_r = \dfrac{Q}{2\pi r b}$, so $r v_r = \dfrac{Q}{2\pi b} = \text{constant}$.

Hence

$$
\frac{1}{r}\frac{\partial (r v_r)}{\partial r} = \frac{1}{r}\frac{\partial}{\partial r}\left(\frac{Q}{2\pi b}\right) = 0
$$

and the cylindrical continuity equation is satisfied.

Velocities:

$$
\begin{aligned}
v_r(0.10) &= \frac{0.04}{2\pi \times 0.10 \times 0.02} = 3.18\ \text{m/s} \\
v_r(0.25) &= \frac{0.04}{2\pi \times 0.25 \times 0.02} = 1.27\ \text{m/s}
\end{aligned}
$$

The velocity falls inversely with radius, as the flow area increases.

**Answer: $v_r = 3.18\ \text{m/s}$ at $r = 0.10\ \text{m}$ and $1.27\ \text{m/s}$ at $r = 0.25\ \text{m}$**

## Check yourself

The answer's key points as multiple-choice questions, with the correct option and why.

1. For steady incompressible flow, the continuity equation in cylindrical coordinates is:
   A. d(v_r)/dr + dv_theta/dtheta + dv_z/dz = 0
   B. (1/r) d(r v_r)/dr + (1/r) dv_theta/dtheta + dv_z/dz = 0
   C. (1/r) d(v_r)/dr + dv_theta/dtheta + dv_z/dz = 0
   D. d(r v_r)/dr + d(r v_theta)/dtheta + d(r v_z)/dz = 0
   Answer: B. The factor r inside the radial term arises because the flow area r dtheta dz grows with r; the tangential term has 1/r from arc length. (Key point: Cylindrical continuity equation)

2. For radial flow between discs of gap b, the radial velocity at radius r is:
   A. Q / (pi r^2)
   B. Q / (2 pi r b)
   C. Q b / (2 pi r)
   D. Q / (2 pi b)
   Answer: B. The flow area at radius r is 2 pi r b, so v_r = Q/(2 pi r b), giving 3.18 m/s at r = 0.10 m. (Key point: Radial velocity between discs)

3. Why is continuity satisfied by v_r = Q/(2 pi b r)?
   A. v_r is constant with r
   B. r v_r is constant, so d(r v_r)/dr = 0
   C. v_theta is large
   D. Q varies with r
   Answer: B. r v_r = Q/(2 pi b) is constant, making (1/r) d(r v_r)/dr zero; velocity falls as 1/r. (Key point: Why continuity is satisfied)

## Related in Fluid Mechanics

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- [Laminar flow between fixed parallel plates](https://www.bctengineer.com/question.md?key=semester_4%2Ffluid_mechanics_mechanical%3Alaminar-flow-between-fixed-parallel-plates) — Fluid Mechanics, chapter 6
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- [Oil flow between fixed plates problem](https://www.bctengineer.com/question.md?key=semester_4%2Ffluid_mechanics_mechanical%3Aoil-flow-between-plates-numerical) — Fluid Mechanics, chapter 6

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