Engineering Tool
Composite Laminate & Resin Calculator.
Accurately calculate theoretical cured laminate thickness, fiber volume fraction (Vf), resin consumption, and finished part weight across carbon fiber, fiberglass, and aramid fabrics.
1. Reinforcement Specification
Step 1Weight of dry reinforcement fabric per square meter.
Total number of fabric layers in laminate schedule.
2. Process & Matrix System
Step 2Higher Vf increases mechanical stiffness-to-weight ratio and reduces excess resin weight.
3. Part Surface & Batch Sizing (Optional)
Step 3Allowance for resin infusion feed lines, spiral wrap, catch pot, and laminate edge trimming (recommended 10–20%).
Real-time micromechanics output
Calculated at target Vf compaction
Material Requirements for Part (1.00 m²)
- Dry Fabric Required:
- 1.60 kg
- Theoretical Resin (Zero Waste):
- 0.93 kg
- Recommended Resin Batch (incl. Waste):
- 1.07 kg
- Finished Part Net Weight:
- 2.53 kg
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Engineering Tool
Governing Micromechanics Principles
In composite manufacturing, single cured ply thickness is governed by the conservation of solid volume under compaction (ASTM D3171 / D2584 standards). Cured ply thickness (t) equals dry fabric areal weight (Aw) divided by fiber density (ρf) and fiber volume fraction (Vf).
1. Single Ply Thickness: t = Aw / (1000 × ρf × Vf) mm
2. Total Laminate Thickness: T = N × t mm
3. Resin Areal Weight: Wr = (Aw / Vf) × (1 - Vf) × (ρr / ρf)