Every downstream prediction depends on the material definition. Separate measured values, fitted model coefficients, estimated properties and illustrative defaults. Record temperature, moisture condition, processing state, units and source with the values rather than treating a material name as a complete specification.
Elastic moduli, Poisson ratios and shear moduli define the stiffness response. Density, heat capacity, conductivity, moisture diffusivity and equilibrium uptake define different physical properties and cannot be inferred from stiffness alone. Orthotropic data must respect reciprocal compliance relationships and a physically admissible stiffness matrix.
Cure and crystallization are internal state variables. Their kinetics, heat release and shrinkage require independent parameter definitions and calibration. A strength allowable does not automatically evolve because the elastic modulus or degree of cure changes. Use only the state dependencies implemented by the selected constitutive branch.
Document the applicable property range and interpolation policy. Extrapolation beyond measured temperatures, moisture levels or strain rates is a separate modeling assumption. Illustrative teaching records should remain labeled throughout the result and report.
2.1 Trusted material data from the source.
06.1 Manuals · read online, preview or download →
Theories / Materials
Prepare traceable engineering records, calibrated thermoset cure kinetics, and semicrystalline thermoplastic crystallization models before the data enters micromechanics, processing, laminate, or structural analyses.
Theory map
Models, equations, figures, and cross-referencesCure, heat, and shrinkage
Connect kinetic rate laws with exotherm, vitrification, diffusion limits, and chemical shrinkage.
Open cure theory →Crystallization and morphology
Resolve Nakamura–Avrami crystallization, latent heat, and crystallization shrinkage for PEEK and PEKK.
Open crystallization theory →Complete reference
One continuous sequence2.2 Thermoset cure kinetics
06.1 Manuals · read online, preview or download →
05.1.2 / Materials
Define calibrated epoxy cure, heat release, and irreversible process shrinkage at the material/ply level before solving the laminate process history. Expand any equation for its physical meaning, variables, units, model connection, and theory source.
State variable and model routing
Degree of cure α is the reacted fraction of the available thermoset chemistry. R15 bounds α to [0,1], prevents reverse reaction, and evaluates kinetics independently at every transport node. Each ply selects its own polymer family and kinetics model in the process definition. Select thermoset cure for a reacting resin or an inert material for a nonreacting layer.
Equation detailsExplanation · variables · model connection · reference+
Converts each calibrated kinetic prefactor and activation energy into a temperature-dependent reaction-rate constant. Absolute temperature must be used.
Model connectionEvaluated from the current thermal iterate before the selected cure law is advanced; it therefore couples cure rate to the transient temperature field.
Theory basisSourour–Kamal cure kinetics
Selectable reaction laws
The model ID chooses one of four rate laws. These laws describe chemistry only after their coefficients have been fit to DSC or equivalent measurements for the actual resin formulation.
Equation detailsExplanation · variables · model connection · reference+
Represents a non-autocatalytic reaction whose rate decreases as the unreacted fraction is consumed.
Model connectionThe nth-order cure law. The returned nonnegative rate is passed to the bounded irreversible state update.
Theory basisThermoset kinetic model basis
Equation detailsExplanation · variables · model connection · reference+
Adds an autocatalytic branch that grows with degree of cure to the nth-order branch, allowing an isothermal rate peak after the reaction begins.
Model connectionThe Kamal–Sourour cure law, also used as the base reaction law before vitrification limitation is applied.
Theory basisSourour–Kamal autocatalytic model
Equation detailsExplanation · variables · model connection · reference+
Uses a single autocatalytic rate constant with reacted- and unreacted-fraction powers. A small positive numerical floor on α prevents a zero-to-a-negative-power singularity.
Model connectionThe Prout–Tompkins cure law. It shares the same bounded state update, heat source, and shrinkage mapping as the other cure laws.
Theory basisNASA composite cure-process formulation
Equation detailsExplanation · variables · model connection · reference+
Suppresses the chemical Kamal–Sourour rate as cure passes a calibrated vitrification threshold. It is an empirical mobility correction, not an independently predicted glass-transition model.
Model connectionThe diffusion-limited cure law. The limited rate, rather than the raw chemical rate, advances α and produces reaction heat.
Theory basisCure-process modeling and vitrification context
Irreversible state integration
Equation detailsExplanation · variables · model connection · reference+
Advances cure over one transport step without consuming more than the remaining unreacted fraction. The outer bounds enforce irreversibility and α≤1.
Model connectionApplied independently at every active thermoset node inside each staggered thermal/kinetic iteration. The reported rate is (αⁿ⁺¹−αⁿ)/Δt.
Theory basisNumerical cure-process integration context
Reaction heat and chemical shrinkage
Equation detailsExplanation · variables · model connection · reference+
Converts cure progress and mass-specific total heat of reaction into a volumetric source for the one-dimensional heat equation.
Model connectionIncluded in the thermal right-hand side only when the cure-exotherm option is enabled and reported separately as cure heat generation.
Theory basisNASA composite cure-process heat balance
Equation detailsExplanation · variables · model connection · reference+
Maps the increase in degree of cure into an anisotropic contraction in the ply material axes. Positive calibrated shrinkage magnitudes therefore produce negative free strain.
Model connectionStored at each process node, fitted across each ply, transformed to laminate axes, and optionally included in the process force and moment resultants.
Theory basisNASA cure-induced residual-stress study
Calibration boundary. Pre-exponential factors, activation energies, exponents, total reaction heat, vitrification controls, and shrinkage are resin-system data. R15 defaults to an inert row and does not represent a universal epoxy.
Material inputs and outputs
| Input family | Purpose | Primary output |
|---|---|---|
| A1, E1, A2, E2, m, n | Temperature-dependent reaction rate | Cure-rate history |
| Hc | Total heat of cure per unit mass | Cure-heat history |
| sc1,2,3 | Full-process local shrinkage magnitudes | Process-shrinkage history |
| α0, αv, sv | Initial state and optional mobility limitation | Degree-of-cure history |
Theory references
2.3 PEEK/PEKK crystallization pipeline
This section describes the coupled material-state formulation. The optional WB5 PEEK parallel and series history models use a different, one-way calculation without latent-heat or shrinkage feedback; see Crystallization consolidation and interface bonding in the processing chapter.
06.1 Manuals · read online, preview or download →
05.1.3 / Materials
Represent calibrated semicrystalline thermoplastic evolution with single- or double-branch Nakamura/Avrami-style kinetics, latent heat, and anisotropic crystallization shrinkage. Expand any equation for its physical meaning, variables, units, model connection, and theory source.
This page describes the coupled material-state formulation. The optional WB5 PEEK parallel and series models use a separate one-way history calculation, without latent-heat or shrinkage feedback. See crystallization, consolidation and interface bonding for those models and their implementation limits.
State normalization and temperature window
Select thermoplastic crystallization for a semicrystalline polymer. Crystallinity X is bounded between its initial value and the user-supplied maximum Xmax. Kinetics are active only when the current nodal temperature lies strictly between the calibrated glass-transition and melting temperatures.
Equation detailsExplanation · variables · model connection · reference+
Expresses current absolute crystallinity as a fraction of the maximum crystallinity available to the selected thermoplastic grade.
Model connectionThe normalized state is used by both Nakamura branches and the bounded integration rule; the crystallinity history retains the absolute crystallinity X.
Theory basisNakamura nonisothermal crystallization
Equation detailsExplanation · variables · model connection · reference+
Combines Arrhenius temperature dependence with a calibrated undercooling function that vanishes at the melting temperature and is evaluated only inside the Tg–Tm process window.
Model connectionEvaluated at every active thermoplastic transport node using the current thermal iterate. Outside Tg<T<Tm, R15 sets the crystallization rate to zero.
Theory basisPEEK dual-mechanism crystallization model
Nakamura/Avrami evolution
Equation detailsExplanation · variables · model connection · reference+
Differentiates the Nakamura form of Avrami crystallization to obtain an instantaneous nonisothermal rate in the normalized state. Numerical floors protect the logarithm near ξ=0 and ξ=1.
Model connectionThe single-branch crystallization law uses its calibrated rate directly. The rate is then advanced using the irreversible bounded update.
Theory basisNakamura rate formulation
Equation detailsExplanation · variables · model connection · reference+
Blends two independently calibrated Nakamura branches to represent two-stage crystallization with one bounded weighting factor.
Model connectionThe dual-branch crystallization law. The same combined rate controls crystallinity growth, latent heat release, and the subsequent shrinkage state.
Theory basisVelisaris–Seferis dual-mechanism PEEK model
Equation detailsExplanation · variables · model connection · reference+
Integrates the normalized rate over the process step without consuming more than the remaining crystallizable fraction, then maps the state back to absolute crystallinity.
Model connectionApplied independently at every active thermoplastic node. The crystallization-rate history reports (Xⁿ⁺¹−Xⁿ)/Δt rather than the normalized branch rate.
Theory basisNonisothermal Nakamura state evolution
Latent heat and crystallization shrinkage
Equation detailsExplanation · variables · model connection · reference+
Converts absolute crystallinity growth and the calibrated heat of crystallization into a volumetric heat source.
Model connectionIncluded in the heat equation only when the crystallization-exotherm option is enabled and reported as crystallization heat generation.
Theory basisPEEK crystallization calorimetry basis
Equation detailsExplanation · variables · model connection · reference+
Maps crystallinity gained after the initial state into an anisotropic contraction in each ply material direction.
Model connectionStored in the process-shrinkage history, fitted through each ply, and optionally added to the laminate process resultants and local failure-stress recovery.
Theory basisProcess-shrinkage residual-stress framework
Material-grade calibration is required. PEEK and PEKK grade, molecular architecture, cooling history, prior melt state, reinforcement, and measurement method change the fitted kinetics. The pipeline is a model family, not a generic property card.
Required validation data
- DSC-derived crystallization rate and heat over relevant cooling/heating histories.
- Tg, Tm, and maximum crystallinity for the selected grade.
- Dilatometry or dimensional data for local crystallization shrinkage.
- Verification against nonisothermal process cycles before residual-stress use.
Theory references
- Nakamura et al., “Some aspects of nonisothermal crystallization of polymers. I,” Journal of Applied Polymer Science 16 (1972) 1077–1091.
- Velisaris and Seferis, “Crystallization kinetics of polyetheretherketone (PEEK) matrices,” Polymer Engineering & Science 26 (1986) 1574–1581.
- NASA composite process modeling reference for coupled heat generation, shrinkage, and residual response.
2.4 AI Import
Theories / 05.1.1 AI Import
Research with ChatGPT. Review sources, units and conditions in Workbench before creating new material records.
Read the step-by-step material import guide ↗
Open Material → Find / Import with AI in Workbench to copy a research prompt, load research JSON, attach local datasheets for comparison, and selectively import reviewed properties. Existing records are not overwritten.
Web search and automatic PDF extraction are not connected inside CDS in this version. Unknown values remain absent; estimates require explicit approval. Save the resulting workspace as CDS_DB and retain original source files separately.
Chapter review
Document the applicable property range and interpolation policy. Extrapolation beyond measured temperatures, moisture levels or strain rates is a separate modeling assumption. Illustrative teaching records should remain labeled throughout the result and report.
Current Workbench model references
These model-specific guides describe the documented Workbench controls. Read their calibration requirements and coupling limits; release notes distinguish announced releases from development previews.
References and source sections
References are retained with the formulations they support. Software instructions describe implementation scope; a cited source does not establish independent validation of a CDS calculation.
- Sourour and Kamal, “Differential scanning calorimetry of epoxy cure: isothermal cure kinetics,” Thermochimica Acta 14 (1976) 41–59.
- NASA, Composite Cure Process Modeling and Simulations using Finite Element Analysis (2016).
- NASA/TM–20205009287, residual stresses induced during matrix cure.
- Nakamura et al., “Some aspects of nonisothermal crystallization of polymers. I,” Journal of Applied Polymer Science 16 (1972) 1077–1091.
- Velisaris and Seferis, “Crystallization kinetics of polyetheretherketone (PEEK) matrices,” Polymer Engineering & Science 26 (1986) 1574–1581.
