Generative AI can produce engineering artefacts, but generation alone does not determine whether or how those artefacts should enter safety-critical workflows. This paper develops a formal framework for assigning AI participation and assurance at the level of individual workflow units. Each unit has a participation and assurance record covering its engineering requirement, an approved operational formalization where applicable, the applicable mechanism, fallback where applicable, evidence obligations and the applicable guarantee, plus a deployment-readiness status. The framework distinguishes deterministic verification, statistically calibrated admission, authorized human judgement supported by AI advice, authorized human adjudication of AI-produced artefacts, retained deterministic tool paths and explicit non-participation; these arrangements carry different kinds of guarantee rather than levels on a common scale. The framework also separates formalization fidelity from verifier soundness, provides a staged classification and readiness procedure, and derives conditions for comparing a gated AI-assisted unit with an incumbent process under recurring-population assumptions. We instantiate and apply the framework in an executed 17-unit wing-spar structural-analysis workflow combining deterministically gated AI-generated CAD, retained deterministic computation and human judgement. The AI-generated CAD program passed all 23 deterministic checks and was admitted at the first attempt. Favourable stress magnitudes did not suffice to pass the stress criteria where the predeclared mesh-convergence evidence was insufficient; those criteria were instead referred to engineering judgement. The case demonstrates selective AI participation and explicit evidence handling at unit level; no claim is made of workflow-level dependability, certification, structural safety or productivity.
Figures & tables
Figure 3.1: Overview of the workflow-unit participation and assurance framework. Regime classification, assurance evidence and deployment readiness are distinct; the regimes carry different guarantee kinds and are not ordered on a scalar assurance scale. Stage 1 (Section 4.2 ) assigns Type D, Type E or C[assist], or passes the unit to Stage 2, which selects the admission rule for units whose deliverable AI may produce. The record box shows the fields of Definition 6 (* where applicable) together with the record’s readiness status. Under a READY record, the prescribed mechanism produces, admits or authorizes the deliverable, or a declared fallback produces it; under a NOT READY record (dashed outline), the existing non-AI process produces it (Definition 15 ). PASS denotes a favourable study outcome label (Section 5.6 ), which readiness does not imply.
Figure 5.1: Executed workflow and regime allocation. AI-generated CAD (Type A) enters only through a deterministic gate (ADMIT/REJECT) with a predeclared bounded fallback; meshing, deck handling, solution, extraction and evaluation use deterministic tools (Type D). Residual CAD adequacy and criteria formalization are C[adjudicate]; adequacy and interpretation judgements are C[assist]. Representative units are shown; the executed set comprises 17 units (A 1, D 6, C[adjudicate] 4, C[assist] 6; no B or E), all READY. Dotted outlines mark mechanisms, not workflow units. The predeclared fallback allowed at most three attempts through a bounded repair loop, then engineer-authored CAD through the same gate, then a recorded halt; it was not invoked.
Workflow unit
AI role in this execution
Regime
Acceptance / execution mechanism
CAD program generation
AI generated the program
A
Deterministic gate measures the produced geometry against an approved operational formalization; admission only if every clause is met; declared fallback
Residual CAD adequacy
AI-generated geometry under review; AI compiled evidence
C[adjudicate]
Study author accepts or rejects the artefact on aspects outside the formalized scope
Mesh generation
None
D
Scripted mesher with frozen quality rules
Solver input-deck generation
None
D
Deterministic deck writer and separate deterministic deck checker
3 levels of quadratic triangular shell elements (3,218 / 12,152 / 47,046 elements); all pass; same-host canonical hashes identical
Solver input decks
Separate deterministic deck checker; regeneration comparison
21/21 pass; byte-identical regeneration
Solver
Pinned binary hash; completion and error/warning record
21/21 complete; no errors or warnings recorded
Numerical integrity
Precision-aware force and moment equilibrium; output-consistency conditions
12/12 linear static jobs pass; all conditions satisfied
Frozen inputs
Hash manifest and solver pin re-verified after the run
61/61 manifest entries and solver binary unchanged (contemporaneous report; later re-hash: Supplement S1.5)
Table 5.2: Execution and integrity evidence.
Figure 5.2: Mesh-convergence evidence under the frozen rule. (a) Medium-to-fine relative change of the tip displacement δtip , the smallest positive buckling factors λ+,min and λ−,min , and the web, flange ( σproj ) and stiffener stress metrics (“S1” in the figure denotes the group-maximum stress rule of the frozen engineering plans; Supplement S5.1), divided by the frozen tolerance (1 % for displacement and buckling factors, 5 % for the stress metrics; dashed line: tolerance). Hatched bars and bold values exceed the tolerance (NOT_CONVERGED): the flange project metric σproj (25.9 %) and the stiffener stress (16.4 %). (b) Stresses at positive ultimate load versus mesh level (3,218 / 12,152 / 47,046 elements): raw flange root-corner maximum (255.1 / 299.3 / 340.2 MPa), flange project metric σproj (medium 182.6, fine 246.5 MPa), stiffener and web peaks, the nominal root reference (171.3 MPa) and Fty = 469 MPa; bold labels mark NOT_CONVERGED quantities. The post-hoc interior-flange diagnostic is not plotted and was not a verdict input. Full values: Supplement S5.
After calibrated metre import, X span = 2.400 m ± 1 × 10 -6 m
V-1
Validity
Fresh-process re-import yields a non-empty shape
V-2
Validity
BRep validity of the compound and every face
Appendix
Table 10
Judgement
Regime
Decision
Residual CAD adequacy
C[adjudicate]
The study author judged the admitted geometry adequate for the study and accepted it with limitations. Defensive code branches unnecessary in the pinned environment were recorded rather than edited, because the predeclared protocol allowed modification only through the repair loop.
Formalization of acceptance criteria
C[adjudicate]
The study author approved the criteria (S5.1) before any result.
Discretization adequacy
C[assist]
The study author accepted the three-level study with limitations. Tip displacement, buckling factors and the web stress converged; flange σproj and the stiffener did not. No further refinement was made within this study.
Analysis adequacy and Q-5
C[assist]
The study author kept Q-5 at ADJUDICATE per the predeclared rule and judged the NLGEOM moment deficit consistent with θ 2 /2 (S6.3). It was not used as release-supporting evidence.
Result interpretation
C[assist]
The study author identified the first buckling mode in both senses as a global lateral-torsional mode of the laterally unrestrained cantilever, so the factors depend on the idealization of tip and lateral restraint.
Response to unresolved stress clauses
C[assist]
Recorded as a limitation, with no design change. Model refinement was deferred to a new versioned iteration, and no criterion was changed.