PreVABS Core Modelling/Meshing

  1. Makoto Ueno


    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

  2. Wenbin Yu

    Can you try the vabs/ANSYS we recently developed


  3. Fang Jiang

    The ANSYS-VABS Graphic User Interface (GUI) Official Release can be downloaded here:

    It requires a membership of the group:

  4. Subramani Anbazhagan


              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.

Add Post

User photo

You must be logged in to comment.

Please keep comments polite and on topic. Offensive posts may be removed.