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- Seeking guidance on manually calculating composite material performance for a Nylon66 structure supporting heavy loads. The box, intended for intermediate storage, will withstand approximately 30,000 N of force, primarily in the Y-direction, with support along the X-direction. Dimensions include 15mm for outer walls and 5mm for ribs. Assistance with simplified calculations and considerations for buckling, bulging, moment, von Mises stress, etc., is appreciated
I've conducted Finite Element Analysis (FEA) tests but have limited experience with composite materials. I need guidance on what calculations to perform manually, as my FEA results yield very small values.
Specifically, I need advice on how to approach analyzing a box filled with ribs. What calculations should I prioritize? The box is intended to support a pipe with a weight of approximately 480 kg per meter in smaller increments at a time, acting as a sort of intermediate storage. Thus, it will be subjected to roughly 30,000 N of total force, with forces primarily in the Y-direction and support along the side walls in the X-direction due to high friction, assuming it's stationary (fixed).
The material I've chosen is Nylon66, as in Inventor, with dimensions of 15mm for the outer walls and upper section, and 5mm for the ribs. I'm also considering simplified calculations where appropriate. Any tips on confirming these calculations? Considerations for buckling, bulging, moment, von Mises stresses, etc.?
Appreciate any help I can get.
Specifically, I need advice on how to approach analyzing a box filled with ribs. What calculations should I prioritize? The box is intended to support a pipe with a weight of approximately 480 kg per meter in smaller increments at a time, acting as a sort of intermediate storage. Thus, it will be subjected to roughly 30,000 N of total force, with forces primarily in the Y-direction and support along the side walls in the X-direction due to high friction, assuming it's stationary (fixed).
The material I've chosen is Nylon66, as in Inventor, with dimensions of 15mm for the outer walls and upper section, and 5mm for the ribs. I'm also considering simplified calculations where appropriate. Any tips on confirming these calculations? Considerations for buckling, bulging, moment, von Mises stresses, etc.?
Appreciate any help I can get.
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