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Hygrothermal Strain⚠ unverified

Mechanical / Composites · Compute the combined thermal and moisture (hygrothermal) free strain

Parameters

InputSymbolUnitDefaultDescription
alphaα1/K1.0Coefficient of thermal expansion, per kelv
delta_TΔTK1.0Temperature change
betaβ1.0Coefficient of moisture expansion (per unit moisture concentration)
delta_MΔM1.0Moisture concentration change (dimensionless mass fraction)
OutputSymbolUnitDescription
resultstrainTotal hygrothermal strain (dimensionless)

The science & history

Understanding the Parameters

Derivation (Approaching a Proof)

Both effects are, to first order, linear in their driving change, by analogy with thermal expansion. Thermal expansion gives a free strain proportional to temperature change, $\varepsilon_T = \alpha\,\Delta T$. Moisture swelling is treated identically: absorbed moisture produces a free strain proportional to the moisture change, $\varepsilon_H = \beta\,\Delta M$.

Because both are small free strains acting on the same material, they superpose (linear kinematics):

$$\varepsilon = \varepsilon_T + \varepsilon_H = \alpha\,\Delta T + \beta\,\Delta M.$$

The formal parallel is exact — moisture concentration plays the role of temperature, and $\beta$ the role of $\alpha$ — which is why the two are combined into a single "hygrothermal" analysis in laminate theory, carrying the same mathematics as thermal residual stress.

Dimensional check. $\alpha\,\Delta T = (1/\text{K})\cdot\text{K}$ = dimensionless; $\beta\,\Delta M$ = (per unit moisture)·(moisture fraction) = dimensionless. Their sum $\varepsilon$ is dimensionless — a strain, as required.

History and Development

Hygrothermal analysis became essential as polymer-matrix composites entered aerospace service, where parts cure hot, cool to ambient (locking in thermal residual stress), and then slowly absorb atmospheric or in-service moisture (adding swelling and, often, relieving some of the thermal stress). Combining thermal and moisture strains into one framework — the "hygrothermal" extension of classical laminate theory (Composite Laminate Theory) — is standard practice, drawing directly on the thermal-stress methods of Thermal Stress and Thermal Stress Index.

Related Concepts: Thermal Stress, Thermal Stress Index, Composite Laminate Theory, Rule of Mixtures transverse, Interlaminar Shear Stress, Poisson Ratio Nu12

Notes: Free (unconstrained) strain; constraint in a laminate → residual hygrothermal stress. Both $\alpha,\beta$ strongly anisotropic (larger transversely). Moisture is the hygroscopic analog of thermal expansion. Reference state = cure temperature, dry. Superposition of two linear free strains.

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