#Naca airfoil generator 6 software#
Permission is hereby granted, free of charge, to any person obtaining a copy of this software and associated documentation files (the "Software"), to deal in the Software without restriction, including without limitation the rights to use, copy, modify, merge, publish, distribute, sublicense, and/or sell copies of the Software, and to permit persons to whom the Software is furnished to do so, subject to the following conditions: Underscore_string is Copyright (c) 2011 Esa-Matti Suuronen is ICanHaz.js is Copyright (c) 2010 Henrik Joreteg (Mustache and Mustache.js are Copyright (c) 2009 Chris Wanstrath (Ruby) and Copyright (c) 2010 Jan Lehnardt (JavaScript) respectively)Ĭalendario is Copyright (c) Codrops 2014 by tympanusĪll the above software components are licensed under the MIT license. Underscore is Copyright (c) 2009-2013 Jeremy Ashkenas, DocumentCloud and Investigative Masonry is Copyright (c) 2013 David DeSandro itter is Copyright (c) 2013 Jordan Boesch JQuery ColorBox is Copyright (c) 2013 Jack Moore JQuery timepicker addon is Copyright (c) 2013 Trent Richardson JQuery is Copyright 2013 jQuery Foundation and other contributors ImagesLoaded is Copyright © 2013 David DeSandro Portions copyright (c) Engine Yard and Andre Arkoīootstrap-select.js is Copyright (C) 2013 bootstrap-selectīackbone.js is Copyright (c) 2010-2013 Jeremy Ashkenas, DocumentCloudĪpple-Style Flip Counter is Copyright (c) 2010 Chris Nanney Ruby gems is Copyright (c) Chad Fowler, Rich Kilmer, Jim Weirich and others. Third-Party Software Credits and Attributions For information about these components, click here: Īutodesk, the Autodesk logo, and Fusion 360 are registered trademarks or trademarks of Autodesk, Inc., and/or its subsidiaries and/or affiliates.Īll other brand names, product names or trademarks belong to their respective holders. This Service may incorporate or use background Autodesk technology components. All rights reserved.Īll use of this Service is subject to the terms and conditions of the applicable Autodesk terms of service accepted upon access of this Service. % c = 1 to simplifiy the equation the chord is set to 1 The implementation in MATLAB looks like this:ī = 1.0 % caution for NON-unity entries change the equation for h However, I am struggling to plot the profile based on the equations given here and here. With the help of Aviation.stackexchange I learned that the A-Version of the profile was created to ease manufacturing by thickening the trailing edge-section (by a straight contour from 80% chord backwards). I would like to calculate the profile NACA 64-2A015. Especially since there were really good answers on the NACA 5-digit-Series airfoil generation. I asked this question over at Aviation.stackexchange but after that I figured it might be better to place it here.
0 kommentar(er)
