# Delamination Growth > Use when you must assess delamination growth in a composite laminate by fracture mechanics: compute the mode I strain energy release rate of a DCB double cantilever beam specimen and the mode II rate of an ENF end-notched flexure specimen from load, crack length and coupon geometry, blend mixed-mode rates with the Benzeggagh-Kenane criterion, and compare the total rate against the critical rate for the onset and growth verdict. Produces G_I, G_II, the mixed-mode ratio, critical rate G_c, onset margin and growth verdict gating the delamination tolerance assessment. Trigger: delamination growth, strain energy release rate, double cantilever beam, end notched flexure, mixed mode fracture, benzeggagh kenane criterion, mode I, mode II. - Skill: `ashfordeou/delamination-growth` (Agent Skill, multi-file: 3 files) - Install (CLI): `npx skillmds@latest add ashfordeou/delamination-growth` - Raw SKILL.md: https://api.skillmd.com/api/skills/ashfordeou/delamination-growth/raw - Safety review: pending - Works with: Claude Code, Claude.ai, OpenAI Codex - Category: Marketing & Growth - License: Apache-2.0 - Author: ashfordeOU (https://skillmd.com/u/ashfordeou) - Updated: 2026-09-17 - Page: https://skillmd.com/skills/ashfordeou/delamination-growth --- # Delamination Growth (structures/composites/delamination-growth) Use when the task is assessing delamination onset and growth in a composite laminate with fracture mechanics rather than ply-level stress criteria: the mode I strain energy release rate of a DCB double cantilever beam coupon and the mode II rate of an ENF end-notched flexure coupon are computed from the applied load, crack length and coupon geometry, the two rates are blended into a mixed-mode condition with the Benzeggagh-Kenane criterion, and the total applied rate is compared against the critical rate to produce the growth verdict. This leaf implements the standard beam-theory delamination model in pure Python, stdlib only. It pairs with structures/composites/failure-criteria (stress-based ply failure at the lamina level, this leaf is fracture-mechanics delamination at the laminate level) and with structures/damage-tolerance/crack-growth (the metallic Paris-law sibling). ## Domain quick reference - DCB mode I rate: G_I = 12 * P^2 * a^2 / (E * b^2 * h^3), where h is the half-thickness of one DCB arm (specimen total thickness 2h), P the applied load, a the crack length, b the width, E the flexural modulus. Units: P in N, lengths in m, E in Pa, G in J/m2. - Compliance form: G_I = 3 * P * delta / (2 * b * a), where delta is the total load-line opening of both arms. With the beam-theory opening delta = 2 * w, one-arm tip deflection w = P * a^3 / (3 * E * I) and arm inertia I = b * h^3 / 12, both forms agree exactly. - ENF mode II rate: G_II = 9 * P^2 * a^2 / (16 * E * b^2 * h^3), h the half-thickness of one ENF half-beam. - Mixed-mode ratio: r = G_II / (G_I + G_II); r = 0 in the unloaded state where both rates vanish. - Benzeggagh-Kenane criterion: G_c = G_Ic + (G_IIc - G_Ic) * r^eta, with G_Ic and G_IIc the mode I and mode II critical rates and eta the B-K exponent. Pure mode I (r = 0) gives G_Ic, pure mode II (r = 1) gives G_IIc. - Onset margin and verdict: margin = G_c - G_T with G_T = G_I + G_II; when G_T >= G_c the total applied rate exceeds the critical rate and delamination onset and growth are predicted. - The relations are standard small-deflection beam theory on an isotropic-equivalent laminate flexural stiffness; the values in the worked example are engineering examples, not a material database. CMH-17 is referenced by name for the test-method context, not reproduced. ## Workflow 1. Fix the coupon states: DCB load p_dcb (N), crack length a_dcb (m), arm half-thickness h_dcb (m), ENF load p_enf, crack length a_enf, half-thickness h_enf, shared width b (m) and flexural modulus e (Pa). The two coupons are separate specimens, so their crack lengths and half-thicknesses are independent. 2. Compute the mode I rate of the DCB coupon with dcb_g1. 3. Cross-check the compliance route with dcb_g1_compliance when the load-line opening delta is measured: the opening equals 2 * w with w = P * a^3 / (3 * E * I) and I = b * h^3 / 12 in the beam model. 4. Compute the mode II rate of the ENF coupon with enf_g2. 5. Form the mixed-mode ratio with mixed_mode_ratio and the critical rate with bk_critical from G_Ic, G_IIc and eta. 6. Compute the onset margin with onset_margin, or run the whole assessment in one call with assess, which returns g1, g2, g_t, ratio, g_c, margin, the growth boolean and the verdict string "delamination-growth" or "no-delamination-growth". 7. Confirm the deterministic checks with the contract test scripts/test_delamination_growth.py. ## Worked example Flexural modulus E = 135e9 Pa, width b = 0.02 m, G_Ic = 250 J/m2, G_IIc = 800 J/m2, eta = 1.5. - DCB at P = 50 N, a = 0.05 m, h = 0.0015 m (total 3 mm): E * b^2 * h^3 = 0.18225, so G_I = 12 * 2500 * 0.0025 / 0.18225 = 411.52 J/m2. At P = 30 N the same coupon gives G_I = 148.15 J/m2. - ENF at P = 500 N, a = 0.03 m, h = 0.0015 m: 16 * 0.18225 = 2.916, so G_II = 9 * 250000 * 0.0009 / 2.916 = 694.44 J/m2. - Compliance cross-check with h = 0.003 m: I = b * h^3 / 12 = 4.5e-11, one-arm tip deflection w = 50 * 1.25e-4 / (3 * 135e9 * 4.5e-11) = 3.429e-4 m, load-line opening delta = 2 * w = 6.859e-4 m. dcb_g1 gives 51.44 J/m2 and dcb_g1_compliance gives 3 * 50 * 6.859e-4 / (2 * 0.02 * 0.05) = 51.44 J/m2; with the exact opening the two forms agree to 1e-6. - Growth case: DCB P = 50 N at h = 0.003 m (G_I = 51.44) with ENF P = 500 N at h = 0.0015 m (G_II = 694.44) gives G_T = 745.89, r = 0.9310, G_c = 250 + 550 * 0.89837 = 744.1 J/m2, margin = -1.76, so growth is predicted: verdict delamination-growth. - No-growth case: DCB P = 30 N at h = 0.003 m (G_I = 18.52) with ENF P = 350 N at h = 0.0015 m (G_II = 340.28) gives G_T = 358.80, r = 0.94841, G_c = 250 + 550 * 0.92361 = 757.98 J/m2, margin = +399.18, so no delamination growth is predicted. ## Pitfalls - Comparing ply-level stress indices to a fracture criterion: this leaf assesses delamination onset by energy release rate at the laminate level; stress-based ply failure (Tsai-Wu, max stress) belongs to failure-criteria, and metallic Paris-law growth to damage-tolerance/crack-growth. - Mixing the coupon half-thicknesses: h is the half-thickness of one DCB arm or ENF half-beam (total specimen 2h); the worked example uses h = 0.0015 m for a 3 mm coupon and h = 0.003 m in the compliance cross-check, and the rate scales as h^-3, so an off-by-two in h shifts G by 8x. - Treating the two coupons as one specimen: the DCB and ENF crack lengths and half-thicknesses are independent inputs; reusing one coupon's geometry for both silently mis-blends the mode ratio. - Trusting one form without the cross-check: the load-squared form and the compliance form agree to 1e-6 only when delta = 2 * w with w = P a^3 / (3 E I) and I = b h^3 / 12, so a measured opening that does not follow the beam model breaks the identity. - Reading the verdict at the boundary: growth is predicted when G_T >= G_c, so a zero or slightly negative margin is a predicted onset; the onset margin is G_c - G_T, not a ratio. - Feeding non-physical coupons: negative loads, zero or negative geometry or modulus, zero or negative critical rates, and a non-positive B-K exponent all raise ValueError. ## Verification - Confirm dcb_g1(50.0, 0.05, 0.02, 0.0015, 135e9) returns 411.52 J/m2 and enf_g2(500.0, 0.03, 0.02, 0.0015, 135e9) returns 694.44 J/m2. - Confirm the compliance-form and load-squared-form DCB rates agree to 1e-6 when delta = 2 * P * a^3 / (3 * E * I), I = b * h^3 / 12. - Confirm the B-K critical rate grows monotonically from G_Ic to G_IIc as the mode II share of G_T rises. - Confirm the growth case returns a negative margin and verdict delamination-growth, and the no-growth case a positive margin and verdict no-delamination-growth. - Confirm every negative load, zero or negative geometry or modulus, zero or negative critical rate, and non-positive B-K exponent raises ValueError. - Run the contract test offline: python3 scripts/test_delamination_growth.py (34 tests, deterministic). ## Related leaves - structures/composites/failure-criteria: stress-based ply failure with Tsai-Wu and max-stress indices, the lamina-level complement to this laminate-level fracture leaf. - structures/composites/cmh17-allowables: the laminate and lamina allowables context behind the critical energy release rates. - structures/damage-tolerance/crack-growth: metallic fatigue crack growth with the Paris law, the metallic analog of growth prediction. - structures/damage-tolerance/residual-strength: remaining strength of a cracked panel once growth tolerance is lost. ## Behavior contract (gate 3) Run the deterministic contract test (stdlib unittest, offline): python3 scripts/test_delamination_growth.py The test covers the DCB mode I rate anchors (411.52 and 148.15 J/m2), the ENF mode II anchors (694.44 and 340.28 J/m2), the compliance-form cross-check at h = 0.003 m (51.44 J/m2 from both forms, exact agreement to 1e-6), load-squared and h-cubed scaling, the mixed-mode ratio including pure mode I, pure mode II and the unloaded state, B-K critical rates for the growth and no-growth cases plus monotonicity and bounds, the onset margins, the full assess verdicts for both worked cases, the report keys, and ValueError rejection of negative loads, zero geometry or modulus, non-positive critical rates and a non-positive B-K exponent. ## Compliance - Standards referenced, not reproduced: CMH-17 (Composite Materials Handbook, sae.org) frames the DCB and ENF test-method context; the energy release rate relations above are standard textbook beam-theory results, summary-only per standards-map.yaml. - compliance: STANDARDS-REF, gated: false.