NEOSOULUS
Mechanical
- May 13, 2012
- 5
Dear All,
I have a structure for which i have carried out frequency response analysis using Hypermesh as pre-processor and NASTRAN as solver. I have the following queries:
1) In the .f06 output file, the principal stresses are not printed.
2) I have used hex-hedral meshing for the entire structure. After carrying out the meshing and frequency response analysis only Normal shear stress are printed. When i use the formula(see attachment) to calculate 3d principal stresses, at some points, i am unable to calculate the angle due to incorrect values(of the terms inside bracket of cos inverse-see attachment). Please tell me how can i resolve this issue? Moreover i have not given any damping value for the material during frequency response.
Please advise.
I have a structure for which i have carried out frequency response analysis using Hypermesh as pre-processor and NASTRAN as solver. I have the following queries:
1) In the .f06 output file, the principal stresses are not printed.
2) I have used hex-hedral meshing for the entire structure. After carrying out the meshing and frequency response analysis only Normal shear stress are printed. When i use the formula(see attachment) to calculate 3d principal stresses, at some points, i am unable to calculate the angle due to incorrect values(of the terms inside bracket of cos inverse-see attachment). Please tell me how can i resolve this issue? Moreover i have not given any damping value for the material during frequency response.
Please advise.