Wing Skin/Flat Panel Compression Limit
Автор: Ultralight Airplane Workshop
Загружено: 2022-10-29
Просмотров: 3666
Описание:
Since we will be carrying some loads through the aluminum skins of the UWS-4 ultralight airplane, we need an estimate of how much compression load the skins can carry before buckling. In this case we will use the wing skins as an example of calculating the buckling load.
Link to the Ultralight Airplane Workshop's books web page, including "Simplified Aircraft Design for Homebuilders""
https://www.ultralightairplaneworksho...
Links:
Youtube Channel: / @designer103
Patreon: / ultralight_airplane_workshop
Facebook: / ultralightairplaneworkshop
Twitter: / designer1032
Website: https://www.UltralightAirplaneWorksho...
FAA AC 103-7: https://www.faa.gov/documentLibrary/m...
Xflr5 software:
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.
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Информация по загрузке:
![Riveting the Top Wing Skins [Sling TSi Build Video # 7]](https://imager.clipsaver.ru/IngyZR_KHj0/max.jpg)
![Aircraft Aluminum and Corrosion [Sling TSi Build]](https://imager.clipsaver.ru/hcgxCII6JpA/max.jpg)
