FuncGenFoil: Airfoil Generation and Editing Model in Function Space

Jinouwen Zhang (Shanghai Artificial Intelligence Laboratory) · Junjie Ren (Fudan University) · Ma Qianhong · Jianyu Wu (Shanghai Jiaotong University) · Aobo Yang (The Hong Kong University of Science and Technology) · Yan Lu (The Chinese University of Hong Kong) · Lu Chen (Fudan University) · Hairun Xie (Shanghai Aircraft Design and Research Institute) · Jing Wang (Huawei Technologies Ltd.) · Miao Zhang (Aalborg University) · Wanli Ouyang (Shanghai AI Lab) · SHIXIANG TANG (The Chinese University of Hong Kong)
aerodynamic shape optimizationaf-200k datasetairfoil geometriesarbitrary-resolution samplingdiscrete point setsdiscrete point-based representationsdiversity increaseempirical evaluationsexpressive powerfunction-space generative modelhigh-fidelity designlabel error reductionparametric representationsresolution adaptabilitysmoothness

Aircraft manufacturing is the jewel in the crown of industry, in which generating high-fidelity airfoil geometries with controllable and editable representations remains a fundamental challenge. Existing deep learning methods, which typically rely on predefined parametric representations (e.g., Bézier curves) or discrete point sets, face an inherent trade-off between expressive power and resolution adaptability. To tackle this challenge, we introduce FuncGenFoil, a novel function-space generative model that directly reconstructs airfoil geometries as function curves. Our method inherits the advantages of arbitrary-resolution sampling and smoothness from parametric functions, as well as the strong expressiveness of discrete point-based representations. Empirical evaluations demonstrate that FuncGenFoil improves upon state-of-the-art methods in airfoil generation, achieving a relative 74.4% reduction in label error and a 23.2% increase in diversity on the AF-200K dataset. Our results highlight the advantages of function-space modeling for aerodynamic shape optimization, offering a powerful and flexible framework for high-fidelity airfoil design.