### Reynolds Number Equation and Review

**Fluid Flow Table of Contents**

Hydraulic and Pneumatic Knowledge

*Reynolds Number Equation and Review*

The flow regime (either laminar or turbulent) is determined by
evaluating the Reynolds number of the flow
refer to (Flow Velocity profiles). The *Reynolds
number*, based on studies of Osborn
Reynolds, is a dimensionless number
comprised of the physical characteristics of the flow. Equation 3-7 is used
to calculate the Reynolds number (N_{R})
for fluid flow.

he Reynolds number is defined as the ratio of inertial forces to viscous forces and consequently quantifies the relative importance of these two types of forces for given flow conditions. Reynolds numbers frequently arise when performing scaling of fluid dynamics problems, and as such can be used to determine dynamic similitude between two different cases of fluid flow. They are also used to characterize different flow regimes within a similar fluid, such as laminar or turbulent flow :

- laminar flow occurs at low Reynolds numbers, where viscous forces are dominant, and is characterized by smooth, constant fluid motion;
- turbulent flow occurs at high Reynolds numbers and is dominated by inertial forces, which tend to produce chaotic eddies , vortices and other flow instabilities.

For practical purposes, if the Reynolds number is less than 2000, the flow is laminar. If it is greater than 3500, the flow is turbulent. Flows with Reynolds numbers between 2000 and 3500 are sometimes referred to as transitional flows. Most fluid systems in nuclear facilities operate with turbulent flow. Reynolds numbers can be conveniently determined using a Moody Chart; an example of which is shown in figure B-1. Additional detail on the use of the Moody Chart is provided in subsequent text.

Click on image to view Moody Chart

#### Reynolds Number for a Pipe or Duct in Imperial Units

The Reynolds number for a pipe or duct can also be expressed in Imperial units

Re = (7745.8) u d / ν

where

Re = Reynolds Number (non dimensional)

u = Velocity (ft/s)

d = Pipe diameter (in)

ν = **Kinematic Viscosity** (cSt) (1 cSt = 10 ^{-6} m^{2}/s )