I'm little confused about the fibre orientation in Cross-sectional lamina schema data file in PreVABS, for example in the case of a biaxial[+45/-45] material we'll have mechanical properties for the biaxial coupon. Do I have give this two fibre orientations or I can use 0 deg since the layer'll be in +45/-45. if I have to provide two or even three orientations in case of a triaxial material, How can I provide that in Cross-sectional lamina schema data file.
Makoto Ueno @ on — Edited @ on
Hello,
Is there a quick and straightforward way to model a solid core that fills the entire interior space of an airfoil section in PreVABS?
Thank you
Wenbin Yu @ on
Can you try the vabs/ANSYS we recently developed
Fang Jiang @ on
The ANSYS-VABS Graphic User Interface (GUI) Official Release can be downloaded here: https://cdmhub.org/resources/991
It requires a membership of the group: https://cdmhub.org/groups/ansysvabsgui
Subramani Anbazhagan @ on
Hello,
I'm little confused about the fibre orientation in Cross-sectional lamina schema data file in PreVABS, for example in the case of a biaxial[+45/-45] material we'll have mechanical properties for the biaxial coupon. Do I have give this two fibre orientations or I can use 0 deg since the layer'll be in +45/-45. if I have to provide two or even three orientations in case of a triaxial material, How can I provide that in Cross-sectional lamina schema data file.
Thank for your time.