The material is a braided carbon fiber composite. The following table provides the material properties of each layer:
| UD Braid and Overlaminate: Linear Elastic Material 1 | |
| 
               Young's Modulus in X direction (GPa)  | 
               160  | 
| 
               Young's Modulus in Y direction (GPa)  | 
               9.7  | 
| 
               Young's Modulus in Z direction (GPa)  | 
               9.7  | 
| 
               Poisson's Ratio (PRXY)  | 
               0.33  | 
| 
               Poisson's Ratio (PRYZ)  | 
               0.28  | 
| 
               Poisson's Ratio (PRXZ)  | 
               0.33  | 
| 
               Shear Modulus GXY (GPa)  | 
               5.9  | 
| 
               Shear Modulus GYZ (GPa)  | 
               4.7  | 
| 
               Shear Modulus GXZ (GPa)  | 
               5.9  | 
| 
              
              
               Deltoid: Linear Elastic Material 2  | |
| 
               Young's Modulus in X direction (GPa)  | 
               9.7  | 
| 
               Young's Modulus in Y direction (GPa)  | 
               152  | 
| 
               Young's Modulus in Z direction (GPa)  | 
               9.7  | 
| 
               Poisson's Ratio (PRXY)  | 
               0.021  | 
| 
               Poisson's Ratio (PRYZ)  | 
               0.33  | 
| 
               Poisson's Ratio (PRXZ)  | 
               0.28  | 
| 
               Shear Modulus GXY (GPa)  | 
               5.9  | 
| 
               Shear Modulus GYZ (GPa)  | 
               5.9  | 
| 
               Shear Modulus GXZ (GPa)  | 
               4.7  | 
| 
              
              
               Panel Braids: Linear Elastic Material 3  | |
| 
               Young's Modulus in X direction (GPa)  | 
               65.8  | 
| 
               Young's Modulus in Y direction (GPa)  | 
               46.1  | 
| 
               Young's Modulus in Z direction (GPa)  | 
               9.7  | 
| 
               Poisson's Ratio (PRXY)  | 
               0.421  | 
| 
               Poisson's Ratio (PRYZ)  | 
               0.48  | 
| 
               Poisson's Ratio (PRXZ)  | 
               0.28  | 
| 
               Shear Modulus GXY (GPa)  | 
               25.8  | 
| 
               Shear Modulus GYZ (GPa)  | 
               4.7  | 
| 
               Shear Modulus GXZ (GPa)  | 
               4.7  | 
For VCCT-based crack-growth simulation, isotropic, orthotropic or anisotropic materials can be used with several fracture criteria (including a user-defined option). Multiple cracks are also allowed.
For this simulation, a linear fracture criterion is defined for crack onset and subsequent crack-growth. The linear option assumes that the fracture criterion is a linear function of the Mode I (GI), Mode II (GII), and Mode III (GIII) energy-release rates, expressed as:
| 
              
              
               Critical Energy-Release Rate  | |
|---|---|
| 
               Critical Mode I energy-release rate, 
                                  | 
               0.3  | 
| 
               Critical Mode II energy-release rate, 
                                  | 
               1.0  | 
| 
               Critical Mode III energy-release rate, 
                                  | 
               1.0  | 
Example 36.1: Defining the Fracture Criterion
C1=0.3 C2=1.0 C3=1.0 TB,CGCR,6,,3,LINEAR ! Linear fracture criterion TBDATA,1,C1,C2,C3 TB,CGCR,7,,3,LINEAR ! Linear fracture criterion TBDATA,1,C1,C2,C3