04.01Lamina / CSV
Constituent-to-ply starter
A compact carbon-fiber and epoxy definition for beginning a continuous unidirectional micromechanics study.
- Fiber and matrix assignment
- Volume fractions
- Model selection
User Manual / Examples / Starter files
Open. Inspect.
Run and adapt.
Download compact input datasets and executable solver examples for micromechanics, laminates, plates, cylinders, and beam sections.
| Field | Stored value |
|---|---|
| Fiber / matrix | Carbon fiber / Epoxy |
| Fiber volume fraction | 0.58 |
| Void volume fraction | 0.02 |
| Model | Continuous unidirectional |
Input preview from cds-lamina-starter.csv. No modulus result is stored in this file.
| Ply | Angle | Thickness |
|---|---|---|
| 1 | 0° | 0.125 mm |
| 2 | 45° | 0.125 mm |
| 3 | -45° | 0.125 mm |
| 4 | 90° | 0.125 mm |
| 5 | 90° | 0.125 mm |
| 6 | -45° | 0.125 mm |
| 7 | 45° | 0.125 mm |
| 8 | 0° | 0.125 mm |
Eight-ply CSV · 1.0 mm total thickness. Thermal and moisture increments start at zero.
| Field | Stored value |
|---|---|
| Radius / length | 250 / 1000 mm |
| Internal pressure | 2.5 MPa |
| Axial force / torque | 0 N / 0 N·m |
| Temperature | 23 °C |
| End condition | Closed |
Input preview from cds-cylinder-load-case.csv. Run a compatible solver to obtain the response.
Starter files
3 direct downloads04.02Laminate / CSV
Symmetric plate layup
An eight-ply quasi-isotropic stacking sequence with orientation, thickness, and environmental fields.
- Eight-ply stack
- Symmetric layup
- Thermal and moisture fields
04.03Structural / CSV
Cylinder pressure case
A starter pressure-vessel case with geometry, pressure, loading, temperature, and end-condition inputs.
- Cylinder geometry
- Pressure and load inputs
- Closed-end condition
Engineering use: Verify units, material provenance, boundary conditions, release compatibility, and governing allowables before using any example in a design decision.