|
[Sponsors] |
April 18, 2017, 00:47 |
composite Layers (Laminate stiffness)
|
#1 |
New Member
Nabeel Yahia
Join Date: Apr 2017
Location: Malaysia
Posts: 7
Rep Power: 9 |
hi,
I am doing my research (fluid induced vibration) using star ccm+, and I want to use composite materials for my pipe. I look to previous papers they use to define the laminate stiffness (A11,D11) , however I could not find a way to key-in those stiffness in starccm+. |
|
April 18, 2017, 01:23 |
|
#2 |
Senior Member
Join Date: Nov 2010
Location: USA
Posts: 1,232
Rep Power: 24 |
STAR-CCM+'s solid mechanics abilities are not really advanced enough for this. You are better off using Abaqus for the solid mechanics and coupling it with STAR-CCM+ for the fluid physics.
|
|
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
[snappyHexMesh] Collapsing layers | RomCFD | OpenFOAM Meshing & Mesh Conversion | 5 | January 18, 2020 02:39 |
[ICEM] Prism layers distorted near trailing edge of blade-Unstructured Mesh | Rohith Giridhar | ANSYS Meshing & Geometry | 3 | June 29, 2015 18:52 |
error messages about blockmeshing and solving | cramsdead | OpenFOAM Pre-Processing | 2 | November 11, 2014 11:53 |
[Other] Meshing Layers over Aerofoil | poloding-along | OpenFOAM Meshing & Mesh Conversion | 5 | April 4, 2014 11:41 |
Fluent diverges when using inflation layers | ziggo | FLUENT | 4 | August 9, 2013 13:11 |