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Use Xfoil polars to calculate c_l, c_d and steering tether forces #72
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Sounds good to me. Suggested input:
Format of the .dat file, describing the wing shape: |
If you look here for example: |
OK, just document somewhere the definition of this file format, for example by using this link: https://m-selig.ae.illinois.edu/ads.html |
Additional remark: The .yaml file with the polars should NOT be in git, but added to .gitignore. It should be autogenerated when the .dat file changes. And are the polars not only valid for a curtain Raynauds number? |
I have changed to using a .csv file for the polars, because it is better suited for the tabular data. |
Better explanation of Re formula here: https://en.wikipedia.org/wiki/Reynolds_number#Flow_around_airfoils |
Solved with ufechner7/KiteUtils.jl#58 |
In order to make the kps4_3l accurate without having to fly a real kite, the Xfoil.jl package should be used to find lift and drag coefficients for different aoa and different steering amounts.
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