# Composite Material Design AI Agent Connect

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

## Overview
- **Category:** engineering
- **Price:** Free
- **Endpoint:** https://edge.vinkius.com/vk_preview_SlQlKvmPK7sVNPYo1QpdGsnephtCo0XfNHADJoFt/ai-agent-connect
- **Tags:** composites, mechanics, materials, aerospace, optimization

## Description

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.

## Tools

### 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

## Prompt Examples

**Prompt:** 
```
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.
```

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

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

**Response:** 
```
The optimal fiber fraction required to achieve a 100 GPa modulus is approximately 0.422.
```

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

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

## Frequently Asked Questions

**How do I calculate the stiffness of a composite?**
You can use the `calculate_composite_properties` tool to find the longitudinal and transverse modulus using the rule of mixtures.

**Can I design multi-layer laminates?**
Yes, use `calculate_laminate_stiffness` to predict the effective stiffness of a stack of layers with specific orientations.

**How do I find the right amount of fiber for a target stiffness?**
The `optimize_fiber_fraction` tool calculates the specific volume fraction required to reach your target modulus.