CCalc - Calculating Reynolds Number for an Impinging Jet

AI Thread Summary
To calculate the Reynolds number for an impinging jet using air, the formula Re = ρu dh / μ is appropriate, where ρ is the density, u is the velocity, dh is the nozzle diameter, and μ is the dynamic viscosity. Given the values μ=1.8*10^-5 kg/ms, ρ=1.2 kg/m3, velocity=90 m/s, and nozzle diameter=15 mm, the calculation can be performed as (1.2 kg/m3 * 90 m/s * 0.015 m) / (1.8*10^-5 kg/ms). It's important to ensure that the final answer is dimensionless, confirming the calculation's validity. The discussion emphasizes the need to use the correct formula based on the specific application.
mm391
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I am trying to work out a reynolds number for an impinging jet using air. If I have:

μ=1.8*10-5 kg/ms
ρ=1.2 kg/m3
Velocity = 90m/s
Nozzle Diameter=15mm

is it Re = ρ u dh / μ

Which is (1.2 kg/m3*90m/s*0.015m)/1.8*10-5 kg/ms

Thanks

M
 
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That depends entirely on the application. That would likely be the most commonly used formulation but there could be others.
 
If that's the data you're given then that's probably the formula you have to use. If you're unsure then check that your final answer is dimensionless i.e. has no units.
 
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