Per-beam yield from the model overrides this.
- Shear on the net section: effective web height of Sec.7 [1.4.7] (opening plus any stiffener cut-out in the same section), A_shr = (h_w + t_f + t_p)·t_w·10−² of [1.4.6], τ_net ≤ C_t·τ_eH.
- Bending on the net section through the opening, Z recomputed with the hole removed — Ch.6 Sec.6 [2.2.2].
- [7.2.3] depth, edge distance, length, spacing of adjacent openings, hole in a bracket.
- [7.3.2] for shell / longitudinal bulkhead / longitudinal girder: 2× opening breadth below the strength deck.
- [7.2.4] + Ch.8 Sec.2 [7.1]: the required depth of the edge stiffener when the limits are exceeded.
- Ch.6 Sec.6 [2.1.2] prescriptive shear area with f_shr of Table 1, as a second opinion where there is no beam model.
- Ch.8 Sec.2 [5.1.1] tripping bracket spacing, since an opening close to the flange weakens its lateral support.
- Secondary (Vierendeel) bending of the strips above and below the opening — a screening calculation, see the note on that panel.
- Web buckling in way of the opening: η_Opening ≤ η_all per Ch.8 Sec.1 Table 1 → DNV-CG-0128 Sec.3 [3.4]. The tool prepares the panels P1/P2 and the stresses that check needs (including τ_av = τ_av,web·h/(h−h_0) of CG-0128 Table 6) but does not evaluate the reduction factors.
- Fatigue of the free edge and of the reinforcement welds.
- Corner radii, edge preparation, local stress concentration.
- The proximity rules of [7.2.1] are a checklist on the detail page, not a calculation: bracket toes, pillars, span ends of floors and girders, narrow cofferdam diaphragms. Aft peak heavy floors in way of the rudder horn (Ch.3 Sec.5 [4.2.2]) and structure under windlass / crane (Ch.11 Sec.2 [5.4.3]) are on that list too.
- Whether the beam model itself is right — spans, fixity, effective breadth.