Pressure Drop & Flow Rate for Oxygen Delivery Tube

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SUMMARY

The discussion focuses on calculating the pressure drop and flow rate for a 50-foot oxygen delivery tube with a 0.1-inch inside diameter. Using Poiseuille's law, the pressure drop formula is defined as ΔP = (8LQμ)/(πR^4), where L is the tube length, Q is the volumetric flow rate, μ is the viscosity, and R is the tube radius. The viscosity of air at room temperature is approximately 17 × 10^-6 Pa·s. A critical point raised is the unrealistic mean flow velocity of 395 m/s at a flow rate of 2 liters per second, suggesting a possible error in the flow rate measurement.

PREREQUISITES
  • Understanding of Poiseuille's law for laminar flow
  • Familiarity with fluid dynamics concepts
  • Knowledge of unit conversions to MKS (meter-kilogram-second) system
  • Basic principles of pressure drop calculations in fluid systems
NEXT STEPS
  • Research the application of Poiseuille's law in real-world scenarios
  • Learn about Bernoulli's equation and its applications in fluid dynamics
  • Explore the effects of tube diameter on flow rates and pressure drops
  • Investigate methods for measuring flow rates accurately in gas delivery systems
USEFUL FOR

This discussion is beneficial for engineers, medical professionals involved in oxygen delivery systems, and anyone interested in fluid dynamics and pressure drop calculations in tubing systems.

wjt
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I am on home oxygen and receive the gas through a 50feet long tube about .1" inside diameter.If the Machine delivers a flow rate of two liters per second, what is the pressure drop through the tubing; What is the flow rate at my end of the tubing?
 
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If Poiseuille flow holds for your system (and it most likely does if the flow is laminar and steady), the relevant formulas are:

\Delta P = \frac{8LQ\mu}{\pi R^{4}}, where

\Delta P is the pressure drop between inlet and outlet, L the length of tube, Q the volumetric flow rate (liters/min, for example), R the tube radius, and \mu the viscosity (in Poise, or equivalent)

So, you have mixed units- convert everything into MKS. Air at room temperature has a viscosity of about 17 *10^-6 Pa*s. Now you can calculate the pressure drop.

The flow rate at the outlet is the same as the inlet- conservation of mass.

If there are viscous losses (entirely possible given the aspect ratio of tubing and flow rate), then YMMV.
 
You can use the Bernoulli losses formula to calculate it.

(\frac{P1}{\gamma} +Z1) -( \frac{P2}{\gamma} +Z2) = \frac{8fLQ^2}{\ g(Pi)^2D^5}

Q is the flow rate.
P is the pressure at point X.
f is the friction factor of the pipe.
L is the length of the tube.
gamma is ro*g.
Z is the elevation at point X.
 
Last edited:
wjt said:
I am on home oxygen and receive the gas through a 50feet long tube about .1" inside diameter.If the Machine delivers a flow rate of two liters per second, what is the pressure drop through the tubing; What is the flow rate at my end of the tubing?

Hi wjt, could you please re-check that data as it seems a bit unreasonable. Fluid at 2L/second through 0.1 inch diameter would give a required mean flow velocity of 395m/s which is supersonic.

In SI units :

Flow Rate, Q = 2E-3 m^3/s
Radius, r = .1 * 2.54E-2 / 2 = 1.27E-3 m
Cross section : A=pi r^2 = 5.07E-6 m^2

Therefore the mean velocity is, Q/A = 395 m/s

Are you sure it's not 2L/min instead of 2L/s ?
 

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