An edge crack of length a in a plate under cyclic stress σ (peak σmax, ratio R) grows by the empirical Paris law:
da/dN = C · (ΔK)^m
ΔK = Y·(σ_max − σ_min)·√(π·a)
K_max = Y·σ_max·√(π·a), Y ≈ 1.12 (edge crack)
Growth is stable until Kmax reaches the material's fracture toughness KIC, at which point the remaining ligament fails catastrophically — a single overload-free run reproduces this "slow creep, then snap" behaviour.
A single high overload cycle (σOL > σmax) leaves behind a plastic zone at the crack tip larger than the one produced by ordinary cycling. Irwin's plane-stress estimate gives the zone radius:
r_p(K) = (1/2π) · (K / σ_y)²
Subsequent (lower) cycles must first re-grow the crack tip through this residual plastic field before returning to their normal rate — this is retardation. The Wheeler model (1972) captures it with a multiplicative factor on the baseline Paris rate:
C_p = [ r_p(a_i) / (a_OL + r_p,OL − a_i) ] ^ m1 while a_i + r_p(a_i) < a_OL + r_p,OL
da/dN (actual) = C_p · C·(ΔK)^m
C_p starts near zero right after the overload (the crack is deep inside the residual plastic field) and rises back to 1 once the growing crack tip escapes that field — producing the visible dip-then-recovery in the da/dN chart. The exponent m1 controls how strong that dip is: larger m1 means sharper retardation.
- Material buttons — switch Paris-law constants C, m, yield strength σy and toughness KIC (illustrative textbook-order values; real alloys vary by heat treatment).
- σmax / R sliders — set the baseline cyclic load.
- Apply Overload Cycle — fires one cycle at σOL = ratio × σmax at the crack's current position, seeding a retardation zone.
- Wheeler exponent — tunes how aggressively the residual plastic zone slows subsequent growth.