Berkeley, CA: Computers and Structures, Inc. Static and Dynamic Analysis of Structures (4th ed.). ![]() Proceedings of the NUMEETA 1985 Conference, Swansea, Wales.Ī comprehensive description can also be found in Dr. Bending and Membrane Elements for Analysis of Thick and Thin Shells. Communications in Applied Numerical Methods, 7(1), 1-9. A Unified Formulation for Triangular and Quadrilateral Flat Shell Finite Elements with Six Nodal Degrees of Freedom. The techniques and formulations involved are adopted from the following publications: ![]() Stresses are calculated as the product of the stress-strain constitutive matrix and the strain vector obtained from joint displacements. Shell stresses may be reviewed in tabular format through Display > Show Tables > Analysis Results > Element Output > Area Output > Table: Element Stresses - Area Shells. How are shell stresses calculated, and can these stresses be compared to the allowable stress of shell material?Īnswer: Yes, the shell stresses obtained using SAP2000 may be compared directly to the allowable stress of the shell material, as this is the essence of Allowable Stress Design (ASD). ![]() ![]() Formulation What is the difference between thick and thin shells?Īnswer: For response, please see the Thin vs.
0 Comments
Leave a Reply. |
AuthorWrite something about yourself. No need to be fancy, just an overview. ArchivesCategories |