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T8 · CompositesPolymer Composites & Fiber EngineeringGATE 2027 Syllabus (XE5)Shop-Floor Standard
Voigt Longitudinal Rule of Mixtures
Predicts the longitudinal elastic modulus (E11 in GPa) of unidirectional fiber reinforced polymer (FRP) composites parallel to fiber axis.
Mathematical Canonical Relation
Plain Formula: E11 = Vf * Ef + (1 - Vf) * Em
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Vf
Range: 0.1 – 0.75 fraction
Ef
Range: 40 – 600 GPa
Em
Range: 1 – 10 GPa
Calculated Engineering Result:
139.4 GPa
Engineering Verification:Calculated using Voigt longitudinal micromechanics model.
When & Where to Apply
Use when designing continuous fiber reinforced structural parts (CFRP, GFRP) loaded along fiber direction.
Common Engineering Pitfalls
- Applying Voigt equation to transverse loading (transverse requires Reuss inverse model)
Physical Assumptions & Validity Limits
- Continuous unidirectional parallel fibers
- Perfect fiber-matrix interfacial bonding
- Isostrain deformation along fiber direction
Variable Symbols, SI Units & Dimensional Specifications
| Symbol | Variable Meaning | SI Unit | Typical Industrial Range |
|---|---|---|---|
| E_{11} | Longitudinal composite modulus | GPa | — |
| V_f | Fiber volume fraction | fraction | 0.60 |
| E_f | Fiber tensile modulus | GPa | 230 |
| E_m | Matrix resin modulus | GPa | 3.5 |
Worked Industrial Numerical Example: Aerospace Carbon/Epoxy Laminate Longitudinal Stiffness
Problem Statement:
Calculate longitudinal modulus E11 for an aerospace grade unidirectional Carbon/Epoxy prepreg laminate with 60 vol% carbon fiber (Ef = 230 GPa) in epoxy matrix (Em = 3.5 GPa).
Step-by-Step Numerical Solution:
- Apply Voigt Model: E11 = (0.60 * 230) + (1 - 0.60) * 3.5
- Fiber contribution = 138 GPa
- Matrix contribution = 1.4 GPa
- Sum contributions: E11 = 138 + 1.4 = 139.4 GPa
Final Answer: E11 = 139.4 GPa
💡 Engineering Interpretation: Longitudinal modulus is 139.4 GPa. Carbon fibers carry 99% of the tensile load, providing high specific stiffness at 1/5th steel density.
Authoritative Technical Reference & Source Provenance
Analysis and Performance of Fiber Composites by B. D. Agarwal & L. J. Broutman (Wiley, 2006), 3rd Edition, Page 75-82.
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