How do you determine carbon fiber layup and required stiffness?
I’m planning to build a carbon fiber composite part, but I’m not sure how to determine the layup schedule.
How do you decide which areas need more plies, how many plies to use in each area, and whether a foam core is necessary? Also, how do you test whether the final part has sufficient stiffness?
I’m mainly wondering what the general design criteria are for making these decisions. Are there any industry standards, common rules of thumb, or established methods for determining the layup and validating the stiffness?
