Complete manuals · download a whole collection

Each collection includes an editable Word manual and its matching searchable PDF, with linked contents, explanatory text, diagrams and references. Theory equations use native Word mathematics. Individual-page PDF buttons remain available.

Complete User Guide148 pages · 10 chapters · Updated 2026-09-18
Getting Started Handbook139 pages · 8 chapters · Updated 2026-09-18
Training & Exercise Manual386 pages · 115 chapters · all 104 exercises · Updated 2026-09-18
Complete Theory Manual255 pages · 56 chapters · Updated 2026-09-18
Models & Workflow Manual85 pages · 9 chapters · Updated 2026-09-18

These are dated reading editions of the public learning content. Interactive studies and account-controlled classroom notes and databases stay online. For current changes, follow the chapter links back to the website.

Current Workbench, reference editions and downloads

Use the online User Guide for current controls, the released model directory for selectable models and compatibility, and the Training Manual for connected exercises. Wider theory references do not mean every formulation is enabled in Workbench.

Dated GUI captures and compiled Web r18 PDF manuals retain their stated scope; they are not a substitute for current hosted Workbench instructions. Find the overview PDF, guides and exercise databases in Your CDS library.

05.6.03 / Structural / Cylinder model 2

Hyer thick laminated cylinder

Resolve the radial coordinate explicitly through every ply so pressure tractions, interlaminar stress, and displacement continuity are retained across a thick laminated wall.

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.

H-01Axisymmetric strain field
εx = ε̄x
εθ = ur(r) / r
εr = dur(r) / dr
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.

VariablesεxUniform generalized axial strainm/murLayerwise radial displacementmrCurrent radial coordinate in the reference wallmεθHoop strainm/mεrRadial strainm/m

Model connectionThese kinematic fields are evaluated separately in each ply while sharing interface displacement constraints.

Theory basisHyer (1988), stress analysis of thick laminated cylinders

H-02Layer constitutive equation
σ(k) = C̄(k)(k) − ᾱ(k)ΔT(k) − β̄(k)ΔC(k)]
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.

Variablesσ(k)Stress vector in ply kPa(k)Transformed 3D ply stiffnessPaᾱ(k)Transformed ply CTE vector1/Kβ̄(k)Transformed moisture-expansion vector1 or concentration basis

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

H-03Radial equilibrium
r/dr + (σr − σθ)/r = 0
rx/dr + τrx/r = 0
Equation detailsExplanation · variables · model connection · reference

Enforces axisymmetric equilibrium through the wall so radial and hoop stress are mechanically compatible in every ply.

VariablesσrRadial normal stressPaσθHoop normal stressPaτrxRadial–axial shear stressPa

Model connectionThe resulting ordinary differential system determines each layer's radial solution coefficients.

Theory basisHyer (1988), radial equilibrium formulation

H-04Interface and pressure boundary conditions
ur(k) = ur(k+1), σr(k) = σr(k+1), τrx(k) = τrx(k+1)
σr(ri) = −pi, σr(ro) = −po
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.

VariablesriCylinder inner radiusmroCylinder outer radiusmpiInternal pressurePapoExternal pressurePa

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 whenUse Hyer cylinder when
Rapid sizing, membrane dominance, and large radius-to-thickness ratioThick walls, strong radial gradients, or interface tractions matter
Hoop/axial resultants are the primary design quantitiesLayerwise 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.