YWS-4 Aero Design: Part 11b, Spanwise Load Distribution with Flaps and Ailerons

We are expanding the flight conditions to explore for the span wise load distribution on the wing of the UWS-4 Ultralight airplane design. In this video more conditions of the flight envelope are added and the conditions for flaps deployed and the ailerons deflected are considered.

We are getting closer to being able to start the design of the spar of the outer wing panel. Woot. Woot.

Link to the Ultralight Airplane Workshop's books web page, including "Simplified Aircraft Design for Homebuilders""
https://www.ultralightairplaneworkshop.com/design-copy

Links:
Youtube Channel: https://www.youtube.com/channel/UCuC7MVr2bBUQ-9xQbg0v82Q
Patreon: https://www.patreon.com/ultralight_airplane_workshop
Facebook: https://www.facebook.com/UltralightAirplaneWorkshop
Twitter: https://twitter.com/Designer1032
Website: https://www.UltralightAirplaneWorkshop.com

FAA AC 103-7: https://www.faa.gov/documentLibrary/media/Advisory_Circular/AC_103-7.pdf

Xflr5 software: http://www.xflr5.com/xflr5.htm

OpenVSP: http://openvsp.org/

Music: https://www.bensound.com

Disclaimer: If you use any of the information that you see on this video on a project of your own, YOU become the engineer and responsible party for your project. It is possible that miscalculations were made in the production of this video. Since you are now the engineer for your project, you must verify the information that you use.

Видео YWS-4 Aero Design: Part 11b, Spanwise Load Distribution with Flaps and Ailerons канала Ultralight Airplane Workshop