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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.
Naca airfoil generator solidworks software#
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. ABSTRACT: The project purpose was to perform flow motion analysis over a NACA 2412 airfoil having air as a fluid using SolidWorks Flow Simulaion. 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. OBJECTIVE: To perform flow simulation over a NACA 2412 airfoil for various angle of attack using Solidworks Flow Simulation and also compare the lift & drag forces. You should always double check the results being output – especially if you are using the results for engineering calculations. The commercial software ANSYS FLUENT is employed to calculate the flow field on an adaptive structured. HOWEVER, AeroToolBox cannot and does not guarantee that the results output from the calculator are correct. This paper employs a multiobjective genetic algorithm (MOGA) to optimize the shape of a widely used wing in ground (WIG) aircraft airfoil NACA 4412 to improve its lift and drag characteristics, in particular to achieve two objectives, that is, to increase its lift and its lift to drag ratio. The tool has been back-tested and checked against the original source. Every effort has been taken to ensure that all the calculations that form part of this tool are correct and accurate.