Wiki Pages (1-8 of 8)

1. Predict failure index and strength ratio of a honeycomb sandwich plate

   Problem Description The failure index and strength ratio of a honeycomb sandwich plate under the biaxial loading condition are predicted using the MSG plate model. For a plate structural...

   https://cdmhub.org/groups/yugroup/wiki/MainPage/ID:Gmsh4SCtutorials/Gmsh:failureindexhoneycomb

2. Predict failure envelope of a fiber-reinforced composite laminate

   Problem Description The failure envelope of a fiber-reinforced composite laminate is predicted using the MSG plate model. The failure envelope is in terms of plate stress resultants (N11 vs N22)...

   https://cdmhub.org/groups/yugroup/wiki/MainPage/ID:Gmsh4SCtutorials/Gmsh:LaminateFailureEnvelope

3. Predict effective failure strength constants of fiber-reinforced unidirectional composites

   Problem Description The effective initial failure strength constants of fiber-reinforced unidirectional composites are predicted using the MSG solid model. A square packed mechanical model is...

   https://cdmhub.org/groups/yugroup/wiki/MainPage/ID:Gmsh4SCtutorials/Gmsh:Predicteffectivefailurestrengthconstants

4. Predict viscoelastic plate properties of a single-layer plain weave laminate

   Problem Description The MSG solid model is used to predict the effective viscoelastic properties of a plain weave composite using a two-step approach. The first step predicts the effective...

   https://cdmhub.org/groups/yugroup/wiki/MainPage/ID:TexGen4SCtutorials/TexGen:TwostephomogenizationforpredictingviscoelasticABDmatricesofasinglelayerplainweavelaminate

5. Predict failure index, strength ratio, and failure envelope of 3D orthogonal woven plate

   Problem Description In this example, failure index, strength ratio, and failure envelope of a 3D orthogonal woven plate are predicted using MSG failure functions. For computing failure index and...

   https://cdmhub.org/groups/yugroup/wiki/MainPage/ID:TexGen4SCtutorials/TexGen:Predictfailureindexstrengthratioandfailureenvelopeof3Dorthogonalwovenplate

6. Predict initial failure strength constants of plain woven composites

   Problem Description Predicting the failure initiation is the first step for many failure analyses of composites. A popular approach is the multiscale failure analysis, which computes the...

   https://cdmhub.org/groups/yugroup/wiki/MainPage/ID:TexGen4SCtutorials/TexGen:Predictinitialfailurestrengthconstantsofplainwovencomposites

7. Predict thermoelastic properties of plain woven composites

   Problem Description The MSG solid model is used to predict the effective thermoelastic properties of a plain weave composite using a two-step approach. This problem is the example 4.1 in the paper...

   https://cdmhub.org/groups/yugroup/wiki/MainPage/ID:TexGen4SCtutorials/TexGen:Twostephomogenizationforpredictingthermoelasticpropertiesofplainwovencomposites

8. Predict elastic properties of plain woven composites

   Problem Description The MSG solid model is used to predict the effective properties of a plain weave composite using a two-step approach. This problem is the first example in the paper “Liu,...

   https://cdmhub.org/groups/yugroup/wiki/MainPage/ID:TexGen4SCtutorials/TexGen:Twostephomogenizationforpredictingelasticpropertiesofplainwovencomposites