Timeline for How to calculate the zero lift drag coefficient for a wing with data from airfoiltools.com?
Current License: CC BY-SA 4.0
4 events
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| Dec 19, 2020 at 11:25 | comment | added | Peter Kämpf | @RemcovanWoerkom I recomment this and this answer. | |
| Dec 19, 2020 at 10:09 | comment | added | Remco van Woerkom | Ahh that makes a lot of sense! Thank you that helps out a ton. However could you elaborate on how the lift coefficent changes over the span of the wing? Or maybe reccomend a paper or article to read that explains this in more detail? I would love to understand it. Thanks!! | |
| Dec 19, 2020 at 6:42 | history | edited | Peter Kämpf | CC BY-SA 4.0 |
added 161 characters in body
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| Dec 19, 2020 at 6:36 | history | answered | Peter Kämpf | CC BY-SA 4.0 |