8:50 I am alarmed that the rib spacing is close up to the halfway point, then sparse further out. It feels like part of the wing is overdesigned, and part is underdesigned. With the power of your software, it should be trivial to distribute the ribs according to the load, instead of some arbitrary parameter.
Nice job!
thank you!
Great work!
thanks
Not sure I see the point of 7050 for the top skins. Top skins are loaded in compression, mostly. It is no better in buckling than 2024.
Thanks for the video!
Was this your personal project or a thesis project?
just a class project
Well done! What grade did you get for this?
an A
@@huskeyengineering2616 Is this Hajia Chen? 😆
8:50 I am alarmed that the rib spacing is close up to the halfway point, then sparse further out. It feels like part of the wing is overdesigned, and part is underdesigned. With the power of your software, it should be trivial to distribute the ribs according to the load, instead of some arbitrary parameter.
Can I get your entire report for the reference as I am working on the similar project i need the reference for design process of structure.
can you please share the report which contains all the process and calculations?
Hi, is there any link to your paper perhaps?
Structure wing for aircraft comercial?
How can I get the datasets?
you dont say something is best in class especially before its even approved hell even atleast built first lol
That's how confident we were! HAHAHAHAHAHAHAHA!
❤🔥🙏
Can I get entire report please
Can you please share the report
Can someone else bring up an idea here?
Who uploaded this, Lol?