11-27-2021, 08:11 PM
You may have to create a simpler test problem so it is easy to work with an evaluate.
Regarding failure and that sort of thing, how much experience do you have with composites and sizing them for aircraft applications? That as a separate and involved topic. You could look at CMH-17 or "Practical Analysis of Aircraft Composites" (that is my book).
Regarding failure and that sort of thing, how much experience do you have with composites and sizing them for aircraft applications? That as a separate and involved topic. You could look at CMH-17 or "Practical Analysis of Aircraft Composites" (that is my book).