Designing an AirfoilĮvery airfoil ever designed has its own specific characteristics, which are its coefficients of Save As: Use this to save an airfoil that was created or modified under a different name.Ĭonvert All Airfoils to Latest Format: Use this for the program to automatically update any airfoils that were designed for X‑Plane version 7 or earlier so they are compatible with the latest version of the simulator.Įxit: Exit Airfoil Maker. Save: Use this to save an airfoil that was created or modified. Open: Use this to open an existing airfoil for viewing or modification. Files are created, loaded, and saved here the only difference is that, instead of text documents, Airfoil Maker is opening and saving files that represent airfoils. The menus of Airfoil Maker are very simple.Ībout: The About menu’s only option, Version, will display the version of the program and check for updates from the website.įile Menu: The file menu works just like the file menu of any word processor or spreadsheet application.
Airfoil tools how to#
This means you are free to copy, share, and adapt the works so long as you give Laminar Research (creators of X-Plane) credit and release your work under a similar license.įor the most part, this manual assumes basic knowledge of the X‑Plane user interface-in particular, it assumes knowledge of how to open and fly an aircraft. This manual, like all X‑Plane documentation, is released under the Creative Commons Attribution-ShareAlike 2.5 license.
Airfoil tools pdf#
For a PDF version of this manual, use an HTML to PDF converter such as. To search for a specific term or set of words, press “ctrl” (“command” on a Mac) + “f” to be taken to the term anywhere in the document. The Table of Contents is also cross-referenced click on the section you’re looking for to travel there instantly. Throughout this text, there will be cross-references to other parts of the manual, as well as hyperlinks to web pages. The latest version of the manual will always be available from the X‑Plane Developer web site. This is version 11.50 of the manual to Airfoil Maker. Last updated: 16 August 2021 About This Manual Stall Minimum and Maximum Angle of Attack.Coefficient of Moment at High-Alpha Change Point.Coefficient of Moment at Low-Alpha Change Point.Coefficient of Moment High-Alpha Change Point.Coefficient of Moment Low-Alpha Change Point.Coefficient of Drag at Angle of Attack of 10 Degrees.Coefficient of Lift at Which Minimum Drag Occurs.Coefficient of Lift Drop from Stall to 20 Degrees.Coefficient of Lift Curvature After the Stall.Coefficient of Lift Immediate Drop at Stall.Coefficient of Lift Curvature Near the Stall.
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