Material Dashboard

Carbon Fibre
\( \rho_{\text{carbon, fiber}} \) Carbon Fiber Density (kg.m3)
View Help Guide
Purpose: Mass Modelling Base
Logic: The volumetric density of the composite material used to synthesize the weight of all structural components.
Type: Manual Entry
Render on Grids: None
Mathematical Formula:
Adjustable User Input
Python Logic: N/A
Live Evaluation: N/A (Input Variable)
\( X_{\text{carbon, fibre}} \) Carbon Fibre Modulus (GPa)
View Help Guide
Purpose: Young's Modulus (E)
Logic: The material stiffness constant used to calculate deflection resistance and structural stability under load.
Type: Manual Entry
Render on Grids: None
Mathematical Formula:
Adjustable User Input
Python Logic: N/A
Live Evaluation: N/A (Input Variable)
\( TL_{\text{carbon, fiber}} \) Carbon Fiber Tensile Limit (MPa)
View Help Guide
Purpose: Ultimate Tensile Strength.
Logic: The material threshold used to size elements subjected to axial pulling or stretching forces.
Type: Manual Entry
Render on Grids: None
Mathematical Formula:
Adjustable User Input
Python Logic: N/A
Live Evaluation: N/A (Input Variable)
\( CL_{\text{carbon, fiber}} \) Carbon Fibre Compressive Limit (MPa)
View Help Guide
Purpose: Ultimate Compressive Strength.
Logic: The material threshold used to size elements subjected to crushing loads or structural buckling.
Type: Manual Entry
Render on Grids: None
Mathematical Formula:
Adjustable User Input
Python Logic: N/A
Live Evaluation: N/A (Input Variable)
\( \varepsilon_{\text{strain, limit}} \) Carbon Fibre Strain Limit (%)
View Help Guide
Purpose: Elastic Threshold.
Logic: Defines the maximum allowable fibre elongation to ensure the housing remains within its linear elastic memory range.
Type: Manual Entry
Render on Grids: None
Mathematical Formula:
Adjustable User Input
Python Logic: N/A
Live Evaluation: N/A (Input Variable)
\( \tau_{\text{carbon, fiber}} \) Carbon Fiber Shear Limit (MPa)
View Help Guide
Purpose: Material Threshold.
Logic: Interlaminar Material Grade Constant shear limit for the CF rod.
Type: Manual Entry
Render on Grids: None
Mathematical Formula:
Adjustable User Input
Python Logic: N/A
Live Evaluation: N/A (Input Variable)
\( \sigma_{\text{material, yield}} \) Carbon Fibre Material Yield Strength (MPa) 598.000000
View Help Guide
Purpose: Ultimate Threshold.
Logic: The calculated peak stress the material can endure before reaching permanent, non-recoverable deformation.
Type: Calculated (Math Output)
Render on Grids: None
Mathematical Formula:
$$\sigma_{\text{material, yield}} = X_{\text{carbon, fibre}} \times 1000 \times \varepsilon_{\text{strain, limit}}$$
Python Logic: v["Carbon Fibre Modulus (GPa)"] * 1000 * v["Strain Limit (%)"]
Live Evaluation: [ROUTE: STATIC/GLOBAL] 230.0000 * 1000 * 0.0026 = 598.0000