New User of Xfoil: Adjusting Measured Cp for Data Match

  • Thread starter micheljoel200
  • Start date
In summary, the user is trying to use xfoil to measure the pressure coefficient of a wind tunnel and is having trouble matching the data. The user has read that they need to correct their measured data, but does not know how to do so.
  • #1
micheljoel200
3
0
i'm a new user of xfoil. I make measurements (Cp) in wind tunnel. But my measured data don't match with the data of xfoil. I use xfoil like my reference.

Which correction can i bring to my measured Cp so that measured and simualation data match together?

Cp = pressure coefficient

thanks

MJ
 
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  • #2


Why do you think that your measures Cp is wrong? It may be that xfoil is not perfect, after all, it is an inviscid panel code with various viscous corrections that can be implemented.

Otherwise it's hard to say much without knowing more about your experiments.
 
  • #3


some reports compare their measured data with simulation data, and they match very well. But before comparaison they brought some correction of their measured data. The problem is that they don't explain very well what they did.
That is why i'searching now for a very example where almost everything is explain. May be someone can help me here.

thx
 
  • #4


Again, the problem isn't necessarily experimental. It very well may be, but no one can help you unless you explain your experimental setup a little bit. For example, details of the wind tunnel, te model, your measurement techniques, etc.
 
  • #5


My wind tunnel has following measure: L= 123 cm, b=61cm, H=31cm.
in the attachment the blue curvature ist from xfoil and the red curvature is from my measurement. There is an offset between the both curvature, i don't know why. I read in book that to match them i need to correct my measured data. But i don't how i can do that.

Please help me.

thx
 

Attachments

  • WIND TUNNEL DATA.xls
    45.5 KB · Views: 189
  • #6


Assuming you have done nothing wrong with your experiment the correction you need to apply is due to tunnel wall effects. To correct the pressure coefficient you have to correct the dynamic pressure for blockage effects. When you place a model in a tunnel you reduce the effective area through which the air can flow and because mass must be conserved the air will speed up. A similar effect is caused by the wake of your model. You probably measure dynamic pressure upstream of your model so the dynamic pressure your model is experiencing is different from what you measure, therefore you have to correct for it. I will not go into how to do this because it would take to long but you should look at "Low Speed Wind Tunnel Testing" by Pope.

However after looking at your data I can tell you that your only problem is not the blockage effects I just explained, unless your model is really big relative to your tunnel in which case you shouldn't be using that model. The difference between your data and xfoil is too large for it to only be blockage effects. So you either did something wrong in your experiment or xfoil.
 

Related to New User of Xfoil: Adjusting Measured Cp for Data Match

1. What is Xfoil and how is it used in scientific research?

Xfoil is a computer program used in aerodynamic research to analyze the performance of airfoils. It uses numerical methods to calculate lift, drag, and other important parameters for a given airfoil shape and operating conditions.

2. How can a new user adjust measured Cp for data match in Xfoil?

To adjust measured Cp (pressure coefficient) for data match in Xfoil, a new user would need to use the "Adjust Cp" feature, which allows the user to input a target Cp value at a specific point along the airfoil. Xfoil will then adjust the flow conditions to match the desired Cp value.

3. What is the importance of adjusting measured Cp for data match in Xfoil?

Adjusting measured Cp for data match in Xfoil is important because it allows for more accurate analysis and comparison of different airfoil designs. By adjusting the Cp values, researchers can ensure that the results are consistent and reliable.

4. Can Xfoil be used for different airfoil shapes and sizes?

Yes, Xfoil can be used for a wide range of airfoil shapes and sizes. It allows for the input of custom airfoil coordinates or the selection of predefined airfoils from a database. This makes it a versatile tool for aerodynamic research.

5. Are there any limitations to using Xfoil for aerodynamic research?

While Xfoil is a powerful tool for aerodynamic research, it does have some limitations. It assumes steady-state flow and does not take into account factors such as turbulence or real gas effects. Additionally, it may not be suitable for very complex or highly unsteady flows.

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