By using this calculator, you as the user expressly agree to the terms of this disclaimer in full. In no circumstance or event shall, or the domain owner associated with the website, be liable for any damages, whether direct or indirect, incidental, special, or consequential arising out the use of or any defect inherent in the software. It is the responsibility of the user to ensure that the correct values have been selected at all times and to cross-reference the results with those contained in the cited references. The entire risk as to the software applicability, performance and quality lies solely with you as the user and not. The use of this software comes with NO WARRANTY or LIABILITY of any kind. 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.Īerotoolbox has made this calculator freely available to use by accessing it from the /naca-4-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. Use the Show Coordinates button to export the resulting coordinate points to a spreadsheet or text editor. The chord can be varied and the trailing edge either made sharp or blunt. Every effort has been taken to ensure that all the calculations that form part of this tool are correct and accurate. The calculator below can be used to plot and extract airfoil coordinates for any NACA 4-series airfoil.
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