Hi i want to model a compsoite shaft of glass/epox and carbon/epox for modal analyse in ansys v12
what element type use ect..
plz help me plzzzzzzzzzzz
By: Payam Soltani, M. Keikhosravy & R. H. Oskouei & C. Soutis
http://www.springerlink.com/content/h831735260162p66/
Abstract:
Numerical simulations based on finite element modelling are increasingly being
developed to accurately evaluate the tensile properties of GLARE (GLAss fibre REinforced
aluminium laminates). In this study, nonlinear tensile behaviour of GLARE Fibre Metal
I am dealing with a partial sphere dome in ANSYS, I created the volume by extruding half of an arch area along the axis at the dome center. I am using SOLID65 elements. The problem I am facing now is how to properly sweep mesh the whole volume ( actually, there are four 90 degree partial sphere together after the extrude of the area), because if I simply sweep the volume, the elements around the top center of the sphere will cause element shape warning in the static analysis.
Dose anyone have any idea about how to deal with the mesh around the center?
Hi everyone,
does anyone know publications dealing with the coupled thermo-structural analysis (direct method) of CFRP using ANSYS?
Hi everyone,
does anyone know publications dealing with the coupled thermo-structural analysis (direct method) of CFRP using ANSYS?
Hi,
I would like to know if there is any chance to simulate orthotropic nonlinear viscoelasticity/creep of CFRP in ANSYS (e.g. by means of user programmable features (UMAT subroutines) or using the software DIGIMAT or others)? For the nonlinear part I would like to use Schapery's method.
Many thanks for yor help!
-André
Hi
Dear friends,
I'm an MSc. student at Bogazici University, Turkiye and I'm working on a thesis project about the failure behaviour of fiber reinforced laminated composite plates under different loading types. The material which we use are AS4 fiber reinforced prepregs and their mechanical properties are the following:
E11 =134,000 MPa
E22 = E33= 9480 MPa
G12 = G13= 5490 MPa
G23 MPa =3272
nu12 = nu13 =0.271
nu23 =0.448
Dear friends,
I'm an MSc. student at Bogazici University, Turkiye and I'm working on a thesis project about the failure behaviour of fiber reinforced laminated composite plates under different loading types. The material which we use are AS4 fiber reinforced prepregs and their mechanical properties are the following:
E11 =134,000 MPa
E22 = E33= 9480 MPa
G12 = G13= 5490 MPa
G23 MPa =3272
nu12 = nu13 =0.271
nu23 =0.448
