Efficient methods to build structural performance envelopes in characteristic load space

• A strategy is proposed and demonstrated to reduce the computational expense of calculating a performance envelope. • A calculation framework is implemented and assessed for the creation of aircraft stiffened panel performance envelopes. • A 43% to 55% reduction in the number of structural evaluations has been demonstrated compared to the previous state-of-the-art. Performance envelopes provide a novel methodology that quantifies the load bearing capacity of a structure in a reduced dimension load space. The envelopes relate the complex loads acting on a structure to the corresponding structural failure constraints and may find many applications within the aircraft structural design process. Constructing envelopes for industrial problems is of particular interest, where the state-of-the-art implementation involves a point cloud meshing and surface modelling strategy. A main challenge in implementing envelopes within an engineering process is the large associated computational costs of construction. The contribution of this article is a robust and efficient strategy to reduce the computational costs of building a performance envelope. The paper presents a method to build the envelopes using a ray-scaling approach. The novel approach is validated by building 3-dimensional envelopes for a representative industrial problem (stiffened panels of AIRBUS’s XRF-1 wing). The results demonstrate a ∼ 42 % reduction in the computation costs compared to the preceding research. The improved construction efficiency makes the employment of envelopes more feasible for large industrial scale processes or when individual failure assessments are computationally expensive.

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Publication Details

Journal
Computers & Structures
Published
2024-11-26
DOI
https://doi.org/10.1016/j.compstruc.2024.107595
Citations
1
Primary Topic
Structural Analysis and Optimization
Type
article
Field-Weighted Citation Impact
0.26

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article

Efficient methods to build structural performance envelopes in characteristic load space

Cecil Armstrong, Adrian Murphy, Sriharsha Sheshanarayana, James Barron et al.
1 citations
Computers & Structures
Structural Analysis and Optimization
0.26
article

Efficient methods to build structural performance envelopes in characteristic load space

Cecil Armstrong, Adrian Murphy, Sriharsha Sheshanarayana, James Barron, N.L. Iorga, Trevor Robinson
article en
1 citations

Abstract

• A strategy is proposed and demonstrated to reduce the computational expense of calculating a performance envelope. • A calculation framework is implemented and assessed for the creation of aircraft stiffened panel performance envelopes. • A 43% to 55% reduction in the number of structural evaluations has been demonstrated compared to the previous state-of-the-art. Performance envelopes provide a novel methodology that quantifies the load bearing capacity of a structure in a reduced dimension load space. The envelopes relate the complex loads acting on a structure to the corresponding structural failure constraints and may find many applications within the aircraft structural design process. Constructing envelopes for industrial problems is of particular interest, where the state-of-the-art implementation involves a point cloud meshing and surface modelling strategy. A main challenge in implementing envelopes within an engineering process is the large associated computational costs of construction. The contribution of this article is a robust and efficient strategy to reduce the computational costs of building a performance envelope. The paper presents a method to build the envelopes using a ray-scaling approach. The novel approach is validated by building 3-dimensional envelopes for a representative industrial problem (stiffened panels of AIRBUS’s XRF-1 wing). The results demonstrate a ∼ 42 % reduction in the computation costs compared to the preceding research. The improved construction efficiency makes the employment of envelopes more feasible for large industrial scale processes or when individual failure assessments are computationally expensive.

Computers & StructuresVol. 306
Airbus (France) (FR), Queen's University Belfast (GB), Airbus (United Kingdom) (GB)
Airbus UK
Affordable and clean energy
Openalex Percentile: Top 43%
Structural Analysis and Optimization
0.26
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