Is Drag Coefficient Constant for same shape, different size?

Click For Summary

Discussion Overview

The discussion revolves around the drag coefficient of objects, specifically spheres, and whether it remains constant when the size of the object changes while keeping other parameters like fluid velocity, density, and viscosity constant. Participants explore the implications of Reynolds number and flow regimes on drag coefficients in different scenarios.

Discussion Character

  • Exploratory
  • Technical explanation
  • Debate/contested

Main Points Raised

  • Some participants question whether "shape" refers solely to geometric shape or if it includes area, particularly when comparing spheres of different radii.
  • It is noted that the drag coefficient can depend on the Reynolds number, which may change with different flow regimes, such as laminar versus turbulent flow.
  • Some argue that if velocity, density, and viscosity are constant, the Reynolds number should not change as long as the testing pipe diameters remain the same.
  • Others clarify that the Reynolds number based on the diameter of the sphere will change with size, and as long as flow regimes remain unchanged, the drag coefficient can be considered approximately constant over a range of sizes.
  • Participants discuss the scalability of drag coefficients and forces for simple shapes like spheres, suggesting that they can often be scaled without significant issues, while more complex shapes may require empirical techniques for accurate scaling.
  • One participant mentions that scaling down models requires maintaining similar Reynolds numbers, which can complicate testing conditions, particularly in supersonic airflow scenarios.

Areas of Agreement / Disagreement

Participants express differing views on the relationship between shape, size, and drag coefficient, particularly regarding the influence of Reynolds number and flow regimes. There is no consensus on whether the drag coefficient remains constant across different sizes of the same shape.

Contextual Notes

Limitations include the dependence on flow conditions and the specific characteristics of the shapes being tested. The discussion highlights the complexity of drag coefficient behavior across different scales and flow regimes.

Typhon4ever
Messages
51
Reaction score
0
I've read that drag coefficient depends on the shape of the object but I am confused as to what shape means. Does it mean geometric shape or is area included in that? Say I have one sphere of radius r and keep fluid velocity, density, and viscosity constant and find its drag coefficient. Would its drag coefficient be different if I measured the drag coefficient of a sphere of radius R assuming again all other parameters are constant?
 
Physics news on Phys.org
It can matter if you change the Reynolds number, e. g. if you change from laminar flow to turbulent flow or vice versa. If that doesn't happen, it is approximately constant if you scale the system up. Wind tunnels usually change more parameters (speed, temperature, ...) to simulate scaled models more accurately.
 
mfb said:
It can matter if you change the Reynolds number, e. g. if you change from laminar flow to turbulent flow or vice versa. If that doesn't happen, it is approximately constant if you scale the system up. Wind tunnels usually change more parameters (speed, temperature, ...) to simulate scaled models more accurately.

If velocity, density, and viscosity are kept constant, would Reynolds number change? It shouldn't as long as the diameters of the testing pipe stay the same right?
 
Typhon4ever said:
I've read that drag coefficient depends on the shape of the object but I am confused as to what shape means. Does it mean geometric shape or is area included in that? Say I have one sphere of radius r and keep fluid velocity, density, and viscosity constant and find its drag coefficient. Would its drag coefficient be different if I measured the drag coefficient of a sphere of radius R assuming again all other parameters are constant?
Shape means the physical geometry of a body. All spheres have the same shape, just different radii.

The drag coefficient is a non-dimensional quantity which relates drag force with other key variables, like fluid velocity, density, and some physical characteristic of the body in question. Different bodies can have different physical characteristics selected for computing drag coefficient. For most simple shapes, like spheres, usually the characteristic chosen is the projected area of the body normal to the flow of the fluid. For other shapes, there may not be such a simple or obvious choice to be made.

Here is a plot of the drag coefficient of a sphere at different Reynold's numbers:

19AFig4.gif

The study of drag coefficients is pretty involved, much too much to be covered in a forum post.

See this article for more discussion:

http://www.thermopedia.com/content/546/?tid=104&sn=1159
 
Typhon4ever said:
If velocity, density, and viscosity are kept constant, would Reynolds number change? It shouldn't as long as the diameters of the testing pipe stay the same right?

If you are doing the test correctly, the diameter Reynolds number of the test section (usually a wind tunnel, not a simple pipe) doesn't matter because it's not a fully-developed duct flow. It's a free stream with thin boundary layers on the walls.

The important parameter here is the Reynolds number based on diameter of the sphere, and that will change with the size. As long as you don't change flow regimes, though, the drag coefficient is essentially constant over several orders of magnitude of ##Re_d##.
 
boneh3ad said:
If you are doing the test correctly, the diameter Reynolds number of the test section (usually a wind tunnel, not a simple pipe) doesn't matter because it's not a fully-developed duct flow. It's a free stream with thin boundary layers on the walls.

The important parameter here is the Reynolds number based on diameter of the sphere, and that will change with the size. As long as you don't change flow regimes, though, the drag coefficient is essentially constant over several orders of magnitude of ##Re_d##.

Just so I am understanding this, by changing the radius of the sphere I am essentially changing the Reynolds number and thus the associated drag force? Are same shaped objects scale-able in terms of their drag force and drag coefficient or would I have to do separate experiments for both?
 
Typhon4ever said:
Just so I am understanding this, by changing the radius of the sphere I am essentially changing the Reynolds number and thus the associated drag force? Are same shaped objects scale-able in terms of their drag force and drag coefficient or would I have to do separate experiments for both?
The Reynolds number is a means to determine what sort of flow regime in which you are performing your test and in which the real article operates. Drag coefficients, as shown in the sketch above, change depending on the Reynolds number of the flow experienced.

The drag of some simple objects, like spheres and cylinders, can be scaled up from model size to full size without too much hassle. Other objects with more complex shapes, like aircraft and ships, can be tested in model form and have their drag scaled up using special empirical techniques, because the Reynolds numbers for the model tests will often be several orders of magnitude smaller than the Reynolds numbers for the full-size article in operation.

It all depends on the shape you are testing and the flow conditions for which you want the full-size drag force.
 
If you scale your model down, you want to keep the Reynolds number similar to the original model. You can reduce the wind speed - but then you increase the Euler number, another relevant dimensionless parameter. In additin, you cannot test supersonic airflow with that approach.
Cryogenic wind tunnels like this one cool down the air to make the tests more realistic in terms of both dimensionless quantities.
 

Similar threads

  • · Replies 1 ·
Replies
1
Views
2K
  • · Replies 14 ·
Replies
14
Views
2K
  • · Replies 28 ·
Replies
28
Views
3K
  • · Replies 6 ·
Replies
6
Views
4K
  • · Replies 1 ·
Replies
1
Views
2K
  • · Replies 13 ·
Replies
13
Views
2K
  • · Replies 11 ·
Replies
11
Views
4K
Replies
5
Views
4K
  • · Replies 9 ·
Replies
9
Views
4K
  • · Replies 17 ·
Replies
17
Views
4K