Calculating Reynolds number in wind tunnel

Click For Summary

Discussion Overview

The discussion revolves around the calculation of Reynolds number in the context of a wind tunnel experiment, specifically for flow over a square cylinder at various angles of attack. Participants explore the relevance of different characteristic lengths and the implications for drag and lift coefficient calculations.

Discussion Character

  • Exploratory
  • Technical explanation
  • Debate/contested
  • Mathematical reasoning

Main Points Raised

  • One participant presents the formula for Reynolds number and discusses the choice of characteristic length, suggesting either the frontal length or hydraulic diameter.
  • Another participant argues that the choice of characteristic length should depend on the specific context of the study, mentioning various possible lengths such as diameter, chord, boundary layer thickness, or roughness height.
  • A participant seeks assistance in verifying a model for flow over a square cylinder, noting a lack of resources for angles of attack other than 0 and 45 degrees.
  • One reply suggests that the relevant Reynolds number for the participant's model is likely based on the length of one side of the square cross-section, or an effective diameter, and recommends consulting literature for conventions in this area.
  • Another participant mentions the importance of literature search for understanding lift and drag calculations on a square cylinder, while expressing limited familiarity with the specific flow problem.
  • A participant indicates that their simulation is steady and laminar, contrasting it with the highly unsteady nature of the phenomenon being studied.

Areas of Agreement / Disagreement

Participants express differing views on the appropriate characteristic length for calculating Reynolds number, indicating a lack of consensus on this aspect. Additionally, there is no agreement on the specific resources or literature that would best support the verification of the model.

Contextual Notes

Participants mention various parameters affecting drag and lift coefficients, such as air speed, square side dimension, and tunnel height, but do not resolve how these factors interact with the Reynolds number calculation.

mostafagemy
Messages
4
Reaction score
0
when calculating a Reynolds number for an obstacle in wind tunnel
Re = air density * air velocity * D / Dynamic viscosity
D here is the characteristic length of the immersed body ( frontal length ) 2 dimensional problem
Or the Hydraulic diameter which relates the tunnel dimensions to the characteristic length of the immersed body ?
 
Physics news on Phys.org
It depends entirely on for what reason what you are calculating the Reynolds number. In general, you won't be using any tunnel dimensions, as almost all interesting quantities are going to be related to the model you are using. Usually the idea is to use the most relevant characteristic length for what you are studying, be it the diameter of your object, the chord of your object, the boundary layer thickness, roughness height or any other number of things.
 
really , I need to verify a model on a program ( flow over a square cylinder with different angles of attack to calc the drag and lift coefficients on it ) . I looked a lot for others work about this problem but what I found was only about 0 and 45 angle of attack , so if u can support me with other web sites , plots or books name , it will be a great help. And thanks for your reply.
 
That would be hard to do without any background on what you a trying to do (and saying you are just verifying a model doesn't really tell me much). For your purpose, the relevant Reynolds number is most likely going to be based on the length of one side of your cross section. I suppose the other option would be finding an effective diameter (similar to the hydraulic diameter of a square tube). I would look into the literature on the subject to figure out what the normal convention is in this case.

For example, perform a search over at JFM:
http://journals.cambridge.org/action/displayJournal?jid=FLM
 
hi boneh3ah ,
I had a network connection problem yesterday

the attached photo is about the model I calculate the Cd & Cl for it.

I'm testing the variation of many parameters on Cd & Cl ( Air speed, square side dimension , tunnel height) also, the shape ( square , triangle)

the fixation points are in the middle of each side ( four fixation points ) & they are also the points which I measure the reaction forces on them.

I'm using Comsol multiphysics program for simulation problem.
thanks a lot
 

Attachments

  • Untitled.png
    Untitled.png
    19.8 KB · Views: 1,117
Like I said, do a search through the literature. I remember seeing a JFM article about calculating lift and drag on a square cylinder, but I personally am not all that familiar with this particular flow problem so I can't tell you all that much.

What I can tell you is that your simulation appears to be steady and laminar based on the wake and this is a highly unsteady phenomenon.
 
thanks a lot for your help boneh3ad
 

Similar threads

  • · Replies 14 ·
Replies
14
Views
3K
  • · Replies 10 ·
Replies
10
Views
3K
Replies
4
Views
6K
  • · Replies 24 ·
Replies
24
Views
42K
Replies
1
Views
5K
  • · Replies 1 ·
Replies
1
Views
3K
  • · Replies 5 ·
Replies
5
Views
4K
  • · Replies 9 ·
Replies
9
Views
4K
  • · Replies 5 ·
Replies
5
Views
2K
Replies
14
Views
6K