MCP For Claude Marketplace
Composite Material Design

Composite Material Design MCP Connector for Claude

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Calculate mechanical properties, optimal fiber content, and laminate stiffness for composite materials.

4 tools Official Updated Oct 1, 2026 Official Vinkius Partner
More Details Connect to Claude

This MCP server provides specialized tools for composite mechanics and material design. Use calculate_composite_properties to determine longitudinal and transverse moduli based on volume fractions. Use optimize_fiber_fraction to find the exact reinforcement needed for a target stiffness. For multi-layer structures, calculate_laminate_stiffness predicts effective stiffness based on ply orientations, while validate_material_compatibility ensures density constraints are met.

compositesmechanicsmaterialsaerospaceoptimization

4 tools expose this connector's capabilities to your AI agent.

calculate_composite_properties

Determines the theoretical mechanical properties of a single-phase composite based on a specific volume fraction

calculate_laminate_stiffness

Predicts the effective stiffness of a multi-layer laminate given different ply orientations

optimize_fiber_fraction

Finds the specific volume fraction of reinforcement required to meet a target stiffness

validate_material_compatibility

Checks if a specific reinforcement and matrix combination is physically viable for a design

See how to talk to your AI agent using Composite Material Design.

Calculate the properties of a composite with a matrix modulus of 3 GPa, reinforcement modulus of 230 GPa, Poisson ratio of 0.3 for both, and a 60% fiber volume fraction.

The longitudinal modulus is 139.2 GPa, the transverse modulus is 3.3 GPa, and the effective Poisson ratio is 0.3.

What fiber fraction is needed to achieve a target modulus of 100 GPa if the matrix is 3 GPa and reinforcement is 230 GPa?

The optimal fiber fraction required to achieve a 100 GPa modulus is approximately 0.422.

Check if a composite with matrix density 1.2 and reinforcement density 1.8 is viable for a max weight of 1.5.

The calculated density is 1.56, which exceeds the maximum allowable weight of 1.5. The material is not viable.

You can use the `calculate_composite_properties` tool to find the longitudinal and transverse modulus using the rule of mixtures.

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