Methodology
The Hyer route follows the generalized-plane-deformation treatment for long laminated cylinders. Each concentric orthotropic ply is transformed into the axial–hoop–radial coordinate system. The solver constructs a layer solution, enforces radial equilibrium inside each ply, applies displacement and traction continuity at every interface, and closes the system with inner and outer pressure boundary conditions.
Equation detailsExplanation · variables · model connection · reference+
Defines the axial, hoop, and radial strains for an axisymmetric cylinder with generalized uniform axial extension and layerwise radial displacement.
Model connectionThese kinematic fields are evaluated separately in each ply while sharing interface displacement constraints.
Theory basisHyer (1988), stress analysis of thick laminated cylinders
Equation detailsExplanation · variables · model connection · reference+
Relates the three-dimensional stress state in each transformed orthotropic ply to mechanical strain after thermal and moisture free strains are removed.
Model connectionThe pristine or damaged per-ply property source is resolved upstream and passed unchanged into this layerwise cylinder branch.
Theory basisCDS independent per-ply material routing
Equation detailsExplanation · variables · model connection · reference+
Enforces axisymmetric equilibrium through the wall so radial and hoop stress are mechanically compatible in every ply.
Model connectionThe resulting ordinary differential system determines each layer's radial solution coefficients.
Theory basisHyer (1988), radial equilibrium formulation
Equation detailsExplanation · variables · model connection · reference+
Closes the multilayer system by preserving radial displacement and traction at ply interfaces and applying pressure tractions at the inner and outer radii.
Model connectionCDS assembles these equations and conditions into one linear coefficient system for the active laminate wall.
Theory basisHyer (1988), layer and surface conditions
Recovered results
The model recovers radial displacement and the axial, hoop, radial, and interlaminar shear stresses at requested through-wall positions. Named results provide the load and resultant histories plus the final radial-coordinate and stress-recovery table.
Selection guidance
| Use shell cylinder when | Use Hyer cylinder when |
|---|---|
| Rapid sizing, membrane dominance, and large radius-to-thickness ratio | Thick walls, strong radial gradients, or interface tractions matter |
| Hoop/axial resultants are the primary design quantities | Layerwise radial displacement and interlaminar stress are required |
Verification basis. Check single-layer isotropic limits, traction continuity, pressure boundary recovery, equilibrium, and convergence of through-wall sampling before using the layerwise solution in design decisions.
Workbench availability: released models, inputs and compatible study paths. The wider theory library includes reference formulations not available in every Workbench solve.
