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 DATABASE 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.
0 kommentar(er)
