LP2SS: Efficient conversion of lamination parameters into stacking sequences using fast Fourier transforms and branch & bound
Fibre-reinforced laminated composites are constructed layer-by-layer, enabling ease of directional stiffness tailoring. Their vast design space is typically explored using two-steps. First, the optimum stiffness for given loads is conceptualised using continuous optimisation of lamination parameters (LPs). Then, discrete optimisation determines a fibre stacking sequence (SS) that closely matches these LPs. While fibre angles are conventionally limited to 45°multiples, finer increments (e.g., ± 15°) can enable lighter structures. However, existing SS design methods do not scale well with this increased problem dimensionality. To overcome this challenge, we propose LP2SS, a novel methodology utilising fast Fourier transforms (FFT) and a branch-and-bound optimiser. By treating LPs as a signal, FFTs identify the number of fibre layers oriented at different angles, akin to estimating the magnitude of different frequencies within a signal. This fibre angle distribution guides the branch-and-bound optimiser, enabling efficient SS design with accurate LP matching, while satisfying empirical design rules. The ingenious use of FFTs is key to LP2SS’s performance, achieving solutions within tenths of a second, compared to minutes required by state-of-the-art methods. Validated on established benchmarks and a newly proposed comprehensive test set, LP2SS marks a significant advancement in the optimal design of large-scale laminated composite structures. • LP2SS: A novel fast Fourier Transform-based approach to design stacking sequences from lamination parameters. • Accurately translates conceptual stiffness into guideline-compliant laminates in few tenths of a second, regardless of laminate size or angle set ( [ Δ 4 5 ∘ ] or [ Δ 1 5 ∘ ] ). • Requires less than 1% of the time taken by state-of-the-art methods for comparable designs. • Introduces new benchmark datasets to evaluate performance on non-conventional [ Δ 1 5 ∘ ] designs.
Authors
- Sascha Dähne (ORCID: https://orcid.org/0000-0003-3497-3225)
- J.M.J.F. van Campen
- Daniël Peeters (ORCID: https://orcid.org/0000-0001-7388-8424)
- Christian Hühne (ORCID: https://orcid.org/0000-0002-2218-1223)
- David Zerbst (ORCID: https://orcid.org/0000-0002-9988-9166)
- R. Manikandan (ORCID: https://orcid.org/0000-0003-1448-7801)
Institutions
- Institute of Flight (US)
- Delft University of Technology (NL)
Publication Details
- Journal
- Composite Structures
- Published
- 2025-12-13
- DOI
- https://doi.org/10.1016/j.compstruct.2025.119939
- Primary Topic
- Composite Structure Analysis and Optimization
- Type
- article
- Field-Weighted Citation Impact
- 0.00