Does the discharge coefficient of an injector depend on the fluid?

Click For Summary
The discharge coefficient, which compares actual discharge to ideal discharge, is influenced by the orifice shape and the fluid's Reynolds number. While an orifice with a rounded inlet approaches a coefficient of 1.0, a square edge inlet typically has a coefficient around 0.61 at high Reynolds numbers. The discharge coefficient is not constant across all incompressible fluids; it varies based on fluid density and behavior. Therefore, if a fluid does not behave like water, its discharge coefficient will differ from that measured with water. Understanding these factors is crucial for accurate fluid dynamics analysis.
Austin_Tx_Rockets
Messages
1
Reaction score
0
TL;DR
If one were to experimentally measure the discharge coefficient using water, would this value be constant for all incompressible fluids?
The discharge coefficient is the ratio of the actual discharge to the ideal discharge and can be measured experimentally. If one were to experimentally measure the discharge coefficient using water, would this value be constant for all incompressible fluids?

What does the discharge coefficient depend on, and is it unique to every fluid?
 
Engineering news on Phys.org
The discharge coefficient is a function of the shape of the orifice and the fluid Reynolds number. An orifice with rounded inlet will have a discharge coefficient approaching 1.0, an orifice with a perfect square edge inlet will have the coefficient approximately 0.61 at high Reynolds numbers. Good search terms to learn more are orifice discharge coefficient and reynolds number. The image below shows the relationship between the discharge coefficient of a square edge orifice with the Reynolds number:
Discharge coefficient.jpg

The discharge coefficient of a specific orifice is unique to the exact shape of the orifice and the Reynolds number.
 
  • Informative
  • Like
Likes gmax137 and Lnewqban
Thread 'Local pressures in turbocharger housing?'
This is question for fluid mechanics. Static pressure in the exhaust manifold(turbo car engine) is usually 1.2 to 2.5 times higher than the boost pressure(intake manifold pressure).Boost pressure is around 1bar guage pressure(2bar absolute). Can the local static pressure somewhere inside a turbine housing ever be lower than atmospheric pressure, is this possible? here some links where CFD is used...

Similar threads

  • · Replies 19 ·
Replies
19
Views
6K
  • · Replies 2 ·
Replies
2
Views
3K
  • · Replies 3 ·
Replies
3
Views
6K
Replies
8
Views
4K
  • · Replies 1 ·
Replies
1
Views
2K
  • · Replies 45 ·
2
Replies
45
Views
5K
Replies
23
Views
2K
  • · Replies 3 ·
Replies
3
Views
2K
Replies
2
Views
2K
  • · Replies 1 ·
Replies
1
Views
1K