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Hi there,
Thank you for the code! I came across with an issue when trying to run it.
for "xfoil.run_result(ali,mach=mach,re=re)", I received error of
"result.read_result(resfilepath)
File C:…
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XFoil error!
Unsuccessful: (0.9714696, 0.9724853) (0.0078040236, -0.0025930437)
Unsuccessful: (0.97357106, 0.9740685) (0.003151073, -0.0071742767)
XFoil error!
Unsuccessful: (0.97616976, 0.9765429…
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Hello,
I tried out the installation guidelines however some kind of CMake error (attached below) still persists. I am trying to download through the base environment of Anaconda3, which uses Python 3…
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Hi, I just install AirPlaneDesign Workbench. when i selected the workbench, receive this error message.
![image](https://user-images.githubusercontent.com/54885418/193453316-6f5fdc82-decd-45b1-a3de-a…
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Is there a way to change the Reynolds number in the analysis?
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I am having an issue when initializing an XFoil object, after a successful installation of the package. Here is the error:
>>> from xfoil import XFoil
>>> xf = XFoil()
Traceback (most recent call…
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Did this with Andrew's data and the BV DS model:
![image](https://cloud.githubusercontent.com/assets/4604869/16432427/f0cd0ac4-3d52-11e6-8a10-66b358643391.png)
The Jacobs data looks like it does rea…
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**Describe the bug**
For time-step simulations, as the design range increases, it seems that the computation time also increases. (as well as the number of iterations). For example, for a 1500 NM ran…
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when i start the tutorial and put "from aeropy.xfoil_module import find_coefficients"
it appears ModuleNotFoundError: No module named 'aeropy.xfoil_module'
how can i solve this problem?
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ncrit is a key parameter of xfoil it is important to be able to set it, the default value of 9 is not always the most adequate setting depending of the usage. gliders will look at values of 10 and abo…