Calculating Air Intake Pressure: A Beginner's Guide

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To calculate the pressure difference in a venturi system, the discharge coefficient (Cv) is essential and varies with geometry and Reynolds number. The standard formula for flow through a venturi is Q = Cv At √(2ΔP/(ρ(1-β^4))), where Q is the volumetric flow rate, At is the throat area, ΔP is the pressure difference, ρ is the flowing density, and β is the diameter ratio. It's noted that for compressible flow, a gas expansion factor may be necessary, but if ΔP is less than 10%, incompressible flow can be approximated. The user confirmed their units for the variables, ensuring they align with the required calculations. Accurate calculations will depend on these parameters and the correct application of the formula.
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(First post!)

The other day I was using my OBD-2 scanner and found out that my car's intake has a peek flow of 25 lbs/min. I converted this to ~317 cubic feet (at 5.5 deg C)

I then calculated the velocity in the 3.5" diameter intake to be ~36 feet/sec.
The intake has a 2" venturi orifice (sound muffler) and calculated the flow at this point to be ~64 feet/sec.

Here is where I am stuck. How do I calculate the pressure difference?

Thank you in advance!
 
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To accurately calculate the expected delta P you need to have the venturi's discharge coefficient. The coefficient is a function of the geometry and is calculated during tests. Venturis usually have pretty high Cv values when compared to an orifice (usually close to 1) but they do vary with Reynolds number.

The standard calculation for flow through a venturi device is

Q = C_v A_t \sqrt{\frac{2 \Delta P}{\rho(1-\beta^4)}}

Where:
Q = Volumetric flow rate
C_v = Discharge coefficient
A_t = Throat area
\Delta P = Pressure difference
\rho = Flowing density
\beta = Diameter ratio
 
Last edited:
I think the standard Cv is taken as 0.975 but varies with the Reynolds number.
 
Just to add my 2 cents...since this is compressible flow, you'll probably need to include a gas expansion factor in Fred's equation. Although, if the delta P is less than 10% (if memeory serves me correctly), Crane TP410 say's that you can use incompressible flow as an approximation. So you'll probably be ok with the first equation.
 
FredGarvin said:
The standard calculation for flow through a venturi device is

Q = C_v A_t \sqrt{\frac{2 \Delta P}{\rho(1-\beta^4)}}

Where:
Q = Volumetric flow rate
C_v = Discharge coefficient
A_t = Throat area
\Delta P = Pressure difference
\rho = Flowing density
\beta = Diameter ratio

Wow! Thanks for the quick replies.

Are my units correct:
Q = Volumetric flow rate in CFM
C_v = Discharge coefficient
A_t = Throat area in inches squared
\Delta P = Pressure difference in inches of water??
\rho = Flowing density in pounds/min
\beta = Diameter ratio 3.5:2
 
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