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Naca airfoil generator software#
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The release of this calculator does not and cannot warrant that any functions contained within are accurate or error free. Be aware that the content on this site is copyrighted and redistribution or copying of this content is prohibited. Finally, if you do discover any bugs in the calculations please send an email to so that a correction can be made.Ī has made this calculator freely available to use by accessing it from the /naca-5-series-airfoil-generator address. You should always double check the results being output – especially if you are using the results for engineering calculations. HOWEVER, AeroToolbox cannot and does not guarantee that the results output from the calculator are correct. The tool has been back-tested and checked against the original source. If you look in The Theory of Wing Sections, there are plots of the chordwise loading provided by different mean lines (camber lines). 2) Chordwise loading is indeed mean line shape. 1) The subscript number has no influence on the airfoil shape description is thus often dropped. Every effort has been taken to ensure that all the calculations that form part of this tool are correct and accurate. RE: Naca 6 Series Airfoil Question 10879353.