Table of Contents
Fetching ...

FeaGPT: an End-to-End agentic-AI for Finite Element Analysis

Yupeng Qi, Ran Xu, Xu Chu

TL;DR

FeaGPT addresses the challenge of fully automating structural FEA workflows from natural language input by introducing a knowledge-augmented Geometry-Mesh-Simulation-Analysis (GMSA) pipeline. The approach combines five integrated stages—planning, geometry generation, adaptive meshing, FEA configuration/execution, and result analysis—driven by LLM planning and vector-based knowledge retrieval with a similarity threshold of $\sigma>0.85$. Key contributions include knowledge-augmented geometry generation, physics-aware adaptive meshing, automated CalculiX configuration, scalable batch processing for parametric studies, and industrial validations on NACA4412 and turbocharger components, demonstrating end-to-end NL-to-FEA automation with reproducible results. This work democratizes access to advanced FEA tools, enabling rapid design space exploration and reliable engineering insights, while laying groundwork for future multi-physics extensions and more complex geometries.

Abstract

Large language models (LLMs) are establishing new paradigms for engineering applications by enabling natural language control of complex computational workflows. This paper introduces FeaGPT, the first framework to achieve complete geometry-mesh-simulation workflows through conversational interfaces. Unlike existing tools that automate individual FEA components, FeaGPT implements a fully integrated Geometry-Mesh-Simulation-Analysis (GMSA) pipeline that transforms engineering specifications into validated computational results without manual intervention. The system interprets engineering intent, automatically generates physics-aware adaptive meshes, configures complete FEA simulations with proper boundary condition inference, and performs multi-objective analysis through closed-loop iteration. Experimental validation confirms complete end-to-end automation capability. Industrial turbocharger cases (7-blade compressor and 12-blade turbine at \SI{110000}{rpm}) demonstrate the system successfully transforms natural language specifications into validated CalculiX simulations, producing physically realistic results for rotating machinery analysis. Additional validation through 432 NACA airfoil configurations confirms scalability for parametric design exploration. These results demonstrate that natural language interfaces can effectively democratize access to advanced computational engineering tools while preserving analytical rigor.

FeaGPT: an End-to-End agentic-AI for Finite Element Analysis

TL;DR

FeaGPT addresses the challenge of fully automating structural FEA workflows from natural language input by introducing a knowledge-augmented Geometry-Mesh-Simulation-Analysis (GMSA) pipeline. The approach combines five integrated stages—planning, geometry generation, adaptive meshing, FEA configuration/execution, and result analysis—driven by LLM planning and vector-based knowledge retrieval with a similarity threshold of . Key contributions include knowledge-augmented geometry generation, physics-aware adaptive meshing, automated CalculiX configuration, scalable batch processing for parametric studies, and industrial validations on NACA4412 and turbocharger components, demonstrating end-to-end NL-to-FEA automation with reproducible results. This work democratizes access to advanced FEA tools, enabling rapid design space exploration and reliable engineering insights, while laying groundwork for future multi-physics extensions and more complex geometries.

Abstract

Large language models (LLMs) are establishing new paradigms for engineering applications by enabling natural language control of complex computational workflows. This paper introduces FeaGPT, the first framework to achieve complete geometry-mesh-simulation workflows through conversational interfaces. Unlike existing tools that automate individual FEA components, FeaGPT implements a fully integrated Geometry-Mesh-Simulation-Analysis (GMSA) pipeline that transforms engineering specifications into validated computational results without manual intervention. The system interprets engineering intent, automatically generates physics-aware adaptive meshes, configures complete FEA simulations with proper boundary condition inference, and performs multi-objective analysis through closed-loop iteration. Experimental validation confirms complete end-to-end automation capability. Industrial turbocharger cases (7-blade compressor and 12-blade turbine at \SI{110000}{rpm}) demonstrate the system successfully transforms natural language specifications into validated CalculiX simulations, producing physically realistic results for rotating machinery analysis. Additional validation through 432 NACA airfoil configurations confirms scalability for parametric design exploration. These results demonstrate that natural language interfaces can effectively democratize access to advanced computational engineering tools while preserving analytical rigor.
Paper Structure (18 sections, 7 equations, 5 figures, 3 tables, 1 algorithm)

This paper contains 18 sections, 7 equations, 5 figures, 3 tables, 1 algorithm.

Figures (5)

  • Figure 1: FeaGPT system architecture illustrating the complete GMSA (Geometry-Mesh-Simulation-Analysis) pipeline. The framework transforms natural language specifications into validated FEA results through intelligent analysis planning, adaptive geometry generation, physics-aware meshing, and solver configuration, with optional data-driven analysis for parametric studies.
  • Figure 2: Geometric details of automatically generated NACA4412 wing structure. (a) Side view showing airfoil profile with NACA4412 camber, inset detail reveals precise spar-shell interface where internal reinforcement integrates with outer skin. (b) Complete 3D assembly demonstrating spanwise ribs intersecting chordwise spars within the cambered shell. (c) Cutaway view exposing internal spar-rib framework, highlighting the automated Boolean operations that resolve complex multi-member intersections without manual intervention.
  • Figure 3: Adaptive mesh generation and FEA results for NACA4412 wing configurations. (a) Automatic mesh refinement showing (i) complete 3D meshed structure, (ii) beam-boundary interface detail, and (iii) NACA4412 airfoil profile view. (b) Von Mises stress distribution showing stress concentrations at spar-root junctions and rib-spar intersections.
  • Figure 4: Comprehensive structural analysis of 432 NACA4412 configurations. (a) Parameter sensitivity showing correlation coefficients between design variables and performance metrics. (b) Weight-stress Pareto front identifying 11 optimal configurations from the design space. (c) Stress distribution across eight-step load spectrum representing typical flight cycles (red dashed line: Al-7075-T6 fatigue limit at 160 MPa). (d) S-N curve for Al-7075-T6 with 432 configuration stress amplitudes overlaid (R=0 pulsating cycle).
  • Figure 5: FEA results from FeaGPT-generated CalculiX configurations for turbocharger components under 110,000 RPM. Compressor (7-blade aluminum rotor): (a-b) von Mises stress distribution (max: 432 MPa at blade roots), (c-d) displacement field (max tip deflection: 0.37 mm). Turbine (12-blade nickel superalloy rotor): (e) stress distribution (peak: 156 MPa), (f) displacement field (max: 0.46 mm). Both show proper cyclic symmetry implementation and realistic structural response.