Rule of Mixtures (transverse)⚠ unverified
Mechanical / Composites · Transverse modulus of a composite (Reuss)
Parameters
| Input | Symbol | Unit | Default | Description |
|---|---|---|---|---|
| Ef | Ef | Pa | 230000000000.0 | Fiber modulus |
| Em | Em | Pa | 3000000000.0 | Matrix modulus |
| Vf | Vf | — | 0.6 | Fiber volume fraction |
| Output | Symbol | Unit | Description |
|---|---|---|---|
| E2 | E2 | Pa | Transverse modulus |
The science & history
Understanding the Parameters
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Matrix modulus $E_m$ dominates — in series, the softest element controls the compliance. Since $E_m \ll E_f$, the transverse modulus is close to (a bit above) the matrix modulus, almost regardless of fiber content.
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Weak $V_f$ dependence — unlike the longitudinal case, $E_2$ rises only slowly with $V_f$; you cannot make a ply stiff transversely just by adding fibers.
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Lower bound and its inaccuracy — the Reuss model is the theoretical lower bound, but it under-predicts real $E_2$ noticeably: it ignores the biaxial constraint the fibers impose on the matrix. Real transverse moduli are higher — use the Halpin-Tsai model (Halpin Tsai Modulus) for accuracy.
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Series analogy — this is the springs-in-series result (compliances add), the transverse counterpart of the parallel longitudinal model (Rule of Mixtures longitudinal).
Derivation (Approaching a Proof)
Load the composite perpendicular to the fibers. Now fiber and matrix layers stack in series along the load, so they carry the same stress $\sigma$ (the iso-stress, or Reuss, assumption) but different strains. Each phase strains by $\varepsilon = \sigma/E$, and the strains combine weighted by volume fraction (the thickness each occupies):
$$\varepsilon_2 = \varepsilon_f V_f + \varepsilon_m(1-V_f) = \sigma\left(\frac{V_f}{E_f} + \frac{1-V_f}{E_m}\right).$$
The composite modulus is $E_2 = \sigma/\varepsilon_2$, so its reciprocal (compliance) is the volume-weighted sum of constituent compliances:
$$\frac{1}{E_2} = \frac{V_f}{E_f} + \frac{1-V_f}{E_m}.$$
The iso-stress assumption is a simplification — in reality the fibers restrain the matrix laterally, raising the true $E_2$ above this bound.
Dimensional check. $\dfrac{1}{E_2} = \dfrac{V_f}{E_f} + \dfrac{1-V_f}{E_m}$ has units $1/\text{Pa}$, so $E_2 = \text{Pa}$ — a modulus, as required.
History and Development
The iso-stress average is August Reuss's (1929) elastic bound, the lower companion to Voigt's upper bound (Rule of Mixtures longitudinal); together they are the Voigt–Reuss bounds of composite stiffness. The transverse rule of mixtures' known inaccuracy motivated the Halpin-Tsai semi-empirical equations (Halpin-Tsai Equations) and rigorous elasticity solutions, which correct for the fiber-constraint effect the simple series model misses.
Related Concepts: Rule of Mixtures longitudinal, Halpin Tsai Modulus, Shear Modulus Inplane, Composite Density, Transverse Strength, Composite Laminate Theory
Notes: Reuss / iso-stress / series model → lower bound, matrix-dominated. Under-predicts real $E_2$ (ignores fiber constraint) — use Halpin Tsai Modulus. Weak $V_f$ dependence; $E_2 \sim 5$–$10\%$ of $E_1$. Same series logic as Shear Modulus Inplane.