keulehans
Aerospace
- Aug 21, 2016
- 8
Hi guys,
I am quite new to Abaqus, so this should be an easy one I hope.
I have two different finished models in Abaqus. The one is an airfoil (without any analyzing) and the other one is a thermally cured fiber reinforced rectangular plate. I performed one analyze step on this plate, in which the plate is cooled down, which leads to residual stresses and Deformation of the plate. The model of the plate works well as the plate behaves as expected.
My Problem now is, that I dont know how I can put together the analyzed (deformed and with residual stresses) rectangular plate and the unanalyzed airfoil. My best guess yet was to import the deformed part from the odb file, but then I only get the deformed mesh without any residual stresses (Composite layup and material is also gone). Also I have to put further analyzing steps onto the model in which both parts are assembled.
Can anyone tell me how I can put together the unanalyzed airfoil and the analyzed rectangular plate, without losing the residual stresses and deformation of the plate?
Thanks very much everyone!
I am quite new to Abaqus, so this should be an easy one I hope.
I have two different finished models in Abaqus. The one is an airfoil (without any analyzing) and the other one is a thermally cured fiber reinforced rectangular plate. I performed one analyze step on this plate, in which the plate is cooled down, which leads to residual stresses and Deformation of the plate. The model of the plate works well as the plate behaves as expected.
My Problem now is, that I dont know how I can put together the analyzed (deformed and with residual stresses) rectangular plate and the unanalyzed airfoil. My best guess yet was to import the deformed part from the odb file, but then I only get the deformed mesh without any residual stresses (Composite layup and material is also gone). Also I have to put further analyzing steps onto the model in which both parts are assembled.
Can anyone tell me how I can put together the unanalyzed airfoil and the analyzed rectangular plate, without losing the residual stresses and deformation of the plate?
Thanks very much everyone!