Been doing a lot of FEA and non-FEA project panel buckling analysis on monolithic composite panels, with all simply supported BC’s. Results acceptable and compare well with in house tools.
When changing Project Sizing- Buckling Tab Boundary Condition all four BC’s from SIMPLE to FIXED, the results are not acceptable and are nowhere near results from in house tools.
The example attached is from an FEA project, with all panels, loading and material properties the same, the only change is from simply supported to fully fixed. For SS, various MS’s but when FF all MS’s are between -0.97 and -0.99. This has been seen on other projects and by other users within my organisation.
Please can you provide some help or advice as to why this is happening and how best to perform fully fixed panel buckling, with confidence in the results. Thanks.