I am trying to do modal analysis of spar. I have modeled flanges using CBEAM and web using CSHEAR elements . I got modal frequencies but I am not sure if they are correct. I found a technical article which tells to use CROD/ extensional stiffness on all 4 sides of CSHEAR as CSHEAR is unstable element. I didn't use CROD/ extensional stiffness in my model. Can anyone guide me on use of CSHEAR elements (should I use CROD)?
My professor has asked me to use CSHEAR element for modeling of spar/rib webs.
Also, the aim is to model whole wing. I have no problem in modeling skins or flanges. However, I am finding it difficult to model CSHEAR elements. Is there any comprehensive tutorial available on use of CSHEARs? Or can you please check the bdf and tell me where I am making mistakes?
My professor has asked me to use CSHEAR element for modeling of spar/rib webs.
Also, the aim is to model whole wing. I have no problem in modeling skins or flanges. However, I am finding it difficult to model CSHEAR elements. Is there any comprehensive tutorial available on use of CSHEARs? Or can you please check the bdf and tell me where I am making mistakes?