HEADFORM 6.5 m/s 142 MPa LAMINATED GLAZING · 6 PLY · 7.06 mm
Automotive · Explicit Dynamics · Composite Failure

Automotive Windshield Impact Reliability — 6-Ply Laminate, Three Load Cases

Explicit dynamics FEA of a 6-ply laminated glazing assembly under pedestrian headform impact, high-velocity stone strike, and post-fracture fragment retention. HIC(d) = 834 (limit 1 000), zero fragments detached, 22% mass-efficient PVB optimum identified — with one design recommendation issued for the 120 km/h stone-strike envelope.

ECE R43 FMVSS 205 JH-2 + XFEM CZM (BK) ANSYS Explicit Prony PVB 2.8M DOF Parametric · 6 variants
Scope a similar study All Case Studies

Project Snapshot

ClientTier-1 Automotive Glazing
ProductLaminated windshield · 7.06 mm
SectorAutomotive · Passive Safety
StandardsECE R43 · FMVSS 205
SolverANSYS Explicit Dynamics
Load cases3 (headform · stone · retention)
Total DOF~2.8 M
Δt explicit~0.05 µs (CFL)
Parametric variants6 (PVB sweep)
HIC(d)834 / 1 000
DeliverableReport + scripts + mesh

2 of 3 load cases pass. 1 design action issued.

LC1 & LC3 cleared · LC2 fails at 120 km/h — TIP redesign recommended
834
HIC(d) — LC1 headform
22% margin to ECE R43 limit (1 000)
4.8 kg sphere · 6.5 m/s · 35°
Compliance: PASS
0
Fragments detached — LC3
Across full thermal range
−40 °C → +80 °C
ECE R43 Annex 3 cleared
0.76 mm
Optimal PVB thickness
HIC(d) = 780 · +18 % mass
Best ROI break-point
22 % compliance margin
120 km/h
Stone-strike penetration
TIP fractures · LC2 FAIL
Design rec. issued:
1.6 → 2.5 mm TIP

Three regulatory impact scenarios. One laminate. Sub-millisecond physics.

The client — a Tier-1 automotive glazing supplier — needed a complete impact-reliability assessment of a new 6-ply laminated windshield assembly before committing tooling. Three regulatory scenarios had to be cleared simultaneously: pedestrian headform impact (ECE R43), high-velocity stone strike (FMVSS 205, 30–120 km/h envelope), and post-fracture fragment retention across a −40 °C to +80 °C thermal range.

The laminate stack — outer glass, two PVB interlayers, inner glass, an EAS/IR functional film, and a chemically strengthened thin inner ply — totals 7.06 mm and combines four distinct constitutive behaviours: brittle fracture, viscoelasticity, cohesive delamination, and pre-stressed chemical tempering. Coupled physics, sub-millisecond timescales, and compliance-grade outputs in a single deliverable.

PVB rate-dependence is the dominant modelling uncertainty. A quasi-static stiffness assumption underestimates peak inner-glass stress by ~35 %. A rate-calibrated Prony series, validated against SHPB data at 100–500 s⁻¹, is mandatory for sub-1 ms impact windows.

Rate-calibrated. Pre-stressed. Cohesively bonded.

SIMFORGE built an explicit dynamics model in ANSYS Explicit Dynamics with a hexahedral-dominant mesh refined to 0.5 mm in the impact zone and graded to 3 mm in the far field. Glass plies use the JH-2 model with XFEM crack enrichment; PVB interlayers use a Prony series calibrated against SHPB data; the chemically tempered TIP is initialised with the residual compressive stress field as an initial condition.

Glass / interlayer interfaces are modelled with a cohesive zone (BK criterion, Gc ≈ 200 J/m²) calibrated against peel and DCB tests. LC3 is a sequential analysis — a static thermal pre-load step feeds the explicit fracture / retention step, with self-contact enabled for post-fracture fragment interaction.

Post-processing is automated through Python (ANSYS ODB API): HIC computation, delamination area tracking, fragment count, and parametric sweep aggregation are all scripted and re-runnable.

Scope of work

Explicit dynamics simulation campaign on a 6-ply laminated windshield with material-model calibration, parametric optimisation of the outer PVB interlayer, and full compliance reporting against two regulatory standards.

Load cases3 — headform impact (LC1), stone strike (LC2), fragment retention (LC3)
Composite stack6 plies — OG · PVB outer · IG · PVB inner · EAS film · TIP
Total thickness7.06 mm nominal
Simulation window0 – 15 ms · Δt ≈ 0.05 µs (CFL-controlled)
Parametric studyPVB outer thickness sweep · 0.38 → 1.00 mm · 6 variants
Standards verifiedECE R43 · FMVSS 205 · EN ISO 3537 · EN 1796
SolverANSYS Explicit Dynamics (Autodyn kernel)
Post-processingPython (ANSYS ODB API) + custom HIC extraction script

Laminate architecture

The six-ply stack is a progressive energy-dissipation system. Each layer performs a distinct structural or functional role — from the sacrificial outer glass to the chemically strengthened inner ply that forms the cabin-side fragment barrier.

← Exterior · Impact face
2.1 mm
Outer glass (OG) — soda-lime silicate, tempered
Sacrificial impact face. Residual compressive stress ~−70 MPa from thermal tempering raises the fracture threshold. First to crack — nucleation occurs on the inner face under bending tension.
E = 70–73 GPa · ρ = 2 500 kg/m³ · Model: JH-2 + XFEM
0.38 mm
PVB — outer interlayer
Primary energy absorber. E ~10 MPa quasi-static → ~700 MPa at impact strain rates (100–500 s⁻¹). Prony series mandatory. CZM interface Gc ≈ 200 J/m² governs fragment retention.
Failure strain 250–350 % · Prony series + CZM (BK criterion)
2.1 mm
Inner glass (IG) — soda-lime silicate, annealed
Structural backbone. Transmits bending load to the A-pillar frame. Sees tensile stress peak after PVB load transfer during headform impact. Equal thickness to OG in this configuration.
E = 70–73 GPa · ρ = 2 500 kg/m³ · Model: JH-2 + XFEM
0.38 mm
PVB — inner interlayer
Secondary bonding and fragment retention layer. Decouples the EAS film thermally and mechanically from IG during thermal cycling (−40 °C to +80 °C). A thinner cross-section is acceptable at this position.
Gc mode I + II · CTE decoupling function
0.50 mm
EAS / IR functional film
IR rejection, HUD compatibility, and antenna integration. Soft (E ~5–20 MPa) with high CTE (~60–80 µm/m·K). Without this compliance buffer, delamination area at −40 °C increases ~3× due to CTE mismatch between TIP and IG.
E = 5–20 MPa · CTE = 60–80 µm/m·K · Model: linear elastic shell
1.6 mm
Thin inner ply (TIP) — chemically strengthened aluminosilicate
Cabin-side fragment barrier. Highest-strength ply in the stack — chemical tempering produces a surface compressive stress of −150 to −300 MPa. Pre-stress must be applied as an initial condition; omitting it under-estimates the fracture threshold by 20–30 %.
E = 72–78 GPa · σ_surf = −150 to −300 MPa (CSG) · IC pre-stress required
Cabin interior →

FEA methodology

Hexahedral-dominant mesh with XFEM crack enrichment, rate-calibrated PVB viscoelasticity, cohesive zone bonding at glass / interlayer interfaces, and pre-stress initial conditions for chemically tempered glass plies.

Mesh parameterValue
Glass element typeC3D8R · 3–5 layers / ply
Impact zone in-plane0.5 mm
Far-field in-plane3 mm · ratio ≤ 1.5
PVB elements2 × C3D8R · AR ≤ 5:1
XFEM enrichment radius30 mm
Total DOF~2.8 M
Δt explicit~0.05 µs (CFL)
Mass scaling zoneFar-field only · factor ≤ 10
Model decisionJustification
JH-2 for glass pliesProgressive damage + residual strength post-fracture
Prony series PVBRate-dependent stiffening 10 → 700 MPa at 500 s⁻¹
CZM interfaceFragment retention energy governed by Gc mode I+II
TIP pre-stress ICσ_surf = −300 MPa — omitting gives 20–30 % threshold error
Thermal pre-load LC3Sequential static step before explicit analysis
Self-contactPost-fracture fragment surface interaction enabled

Load case definition

Three scenarios cover the regulatory envelope: pedestrian protection (LC1), durability (LC2), and post-fracture safety (LC3). Each load case has its own constitutive emphasis and output set.

LC1 — Headform impactECE R43
Impactor mass4.8 kg HIC sphere
Impact velocity6.5 m/s
Impact angle35° to normal
CriterionHIC(d) ≤ 1 000
OutputsHIC · crack map · deflection
LC2 — Stone strikeFMVSS 205
Projectile5 g sphere · ∅3.2 mm
Velocity range30 – 120 km/h
CriterionNo full penetration
OutputsCrack radius · spall zone
120 km/hFAIL → design rec.
LC3 — Fragment retentionECE R43 Annex 3
Temperature range−40 °C → +80 °C
SequenceThermal → fracture → CZM
CriterionNo sharp fragment detach
OutputsDelam. area · peel force
ResultPASS — all temperatures

Simulation results

LC1 headform impact at 6.5 m/s achieves full compliance with 22 % margin. LC2 stone strike passes up to 80 km/h; 120 km/h penetrates the TIP and triggers a design recommendation. LC3 fragment retention passes across the full −40 °C to +80 °C thermal range.

OutputValueLimitStatus
HIC(d) — LC1 · 6.5 m/s8341 000PASS ✓
Peak principal stress — OG inner face142 MPaMonitored
Crack initiation time — OG0.31 ms
PVB peak strain — LC1187 %250–350 %PASS ✓
Max CZM delamination area — LC1410 mm²
Peak panel deflection — LC122.4 mm
Stone strike — 30 km/hNo fractureNo penetrationPASS ✓
Stone strike — 80 km/hContained · TIP intactNo penetrationPASS ✓
Stone strike — 120 km/hTIP fracture · penetrationNo penetrationFAIL ✗
Fragment detachment — −40 °CNoneNonePASS ✓
Fragment detachment — +80 °CNoneNonePASS ✓
ECE R43 fragment countCompliantCompliantPASS ✓
Design recommendation — LC2 @ 120 km/h Increase TIP thickness from 1.6 mm to 2.5 mm, or substitute the inner PVB interlayer with an acoustic-grade variant offering higher storage modulus in the 1–10 kHz impact frequency range. Both options were sized in a follow-on engagement; the 2.5 mm TIP delivers a +2.1 % mass penalty for full LC2 compliance up to 130 km/h.

Parametric study — PVB thickness sweep

Six explicit variants sweeping outer PVB thickness from 0.38 mm (baseline) to 1.00 mm were run to quantify HIC(d) reduction versus added mass. The optimum sits at 0.76 mm: HIC(d) = 780 with only +18 % mass, giving 22 % margin to the ECE R43 limit. Beyond 0.89 mm the marginal HIC gain per gram inverts the mass-efficiency ROI.

HIC(d) vs PVB outer thickness — vertical line = ECE R43 limit (1 000)
★ Optimal: 0.76 mm → HIC(d) = 780 · +18 % mass · 22 % margin · best ROI break-point
PVB thicknessHIC(d)Mass penaltyStatus
0.38 mm — baseline1 010FAIL ✗
0.50 mm965+8 %FAIL ✗
0.64 mm920+14 %FAIL ✗
0.76 mm ★ optimal780+18 %PASS ✓
0.89 mm730+25 %PASS ✓
1.00 mm710+32 %PASS ✓

Key findings

Four conclusions transferred directly into the client's material model card library and laminate specification template — re-usable across the next two glazing programs.

01

PVB rate-dependence is the #1 fidelity driver

Quasi-static PVB stiffness underestimates peak inner-glass stress by ~35 %. A Prony series calibrated at 100–500 s⁻¹ from SHPB data is mandatory for sub-1 ms impact windows. Anything else gives false-positive compliance verdicts.

02

Delamination absorbs 38 % of impact energy

CZM delamination at the OG / PVB interface is the dominant energy sink in LC1. Increasing interface Gc via adhesion-promoter treatment is more mass-efficient than adding glass thickness — a finding that re-frames future design DOEs.

03

TIP pre-stress initial condition is non-negotiable

Omitting the chemical-tempering residual stress (−150 to −300 MPa) underestimates the fracture threshold by 20–30 %. The result is false-conservative crack maps and incorrect compliance verdicts in opposite directions on different load cases.

04

EAS film prevents 3× delamination growth at −40 °C

The film's compliance buffers the CTE mismatch between TIP (aluminosilicate) and IG (soda-lime). Removing it from the LC3 model triples predicted delamination area at the minimum service temperature — a result with direct functional-stack design implications.

Project deliverables

Full traceable documentation package — re-runnable, re-usable, and structured for direct integration into the client's homologation file.

DeliverableFormat
FEA simulation report — methodology, results, compliance matrixPDF / DOCX
Crack-propagation maps — all load casesPNG · ANSYS result files
HIC time-history plots — LC1PDF
Parametric sweep summary — PVB optimisationExcel + PDF
Python post-processing scripts (HIC extractor, delam tracker).py (documented)
Mesh files + material library (Prony, JH-2 constants).inp / .dat

Tools used

Production-grade explicit dynamics workflow built around ANSYS, with custom Python automation for compliance metrics and material-card calibration.

ToolUsage
ANSYS Explicit DynamicsPrimary solver — Autodyn kernel
Python + ANSYS ODB APIHIC computation · delamination tracking · sweep aggregation
HyperMeshPre-processing — hex-dominant meshing, XFEM zone definition
CATIA / SpaceClaimCAD geometry preparation, curvature mapping
MATLABProny series calibration from DMA / SHPB data
DIC (Vic-3D)PVB biaxial strain field validation data
Why SIMFORGE for this type of study

Material-model calibration, explicit dynamics, and compliance reporting in a single engagement. Physics-accurate Prony / JH-2 / CZM card libraries — re-usable across your next glazing programs. Fixed fee, single delivery cycle.

Scope a project

Impact reliability to qualify.
Standard to satisfy. Tell us the laminate.

From laminated glazing to CFRP composites and bonded assemblies — if it needs explicit dynamics, fracture mechanics, or compliance verification against ECE, FMVSS, ISO, or internal OEM specs, we scope it in a 30-minute call and deliver a fixed-fee proposal within 48 hours.

Scope an impact study Automotive capabilities

Initial response · 24 h  ·  NDA available  ·  Fixed-fee proposal within 48 h