A high-temperature aerodynamic non-equilibrium factor correction method based on microcosmic data
By using a non-equilibrium factor correction method based on microdata and employing conditional variational autoencoders and symbolic regression partitioning to fit model parameters, the problems of insufficient prediction accuracy and physical interpretability in high-temperature regions are solved, and high-precision simulation of hypersonic flow fields is achieved.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- COMP NETWORK INFORMATION CENT CHINESE ACADEMY OF SCI
- Filing Date
- 2025-12-31
- Publication Date
- 2026-07-14
AI Technical Summary
Existing computational fluid dynamics models for engineering have poor prediction accuracy in the high-temperature region, and purely data-driven models lack physical interpretability and generalization ability, making it difficult to accurately describe high-temperature aerodynamic non-equilibrium effects.
By constructing a high-temperature aerodynamic non-equilibrium factor correction method based on microscopic data, using a conditional variational autoencoder to learn the data distribution, and combining symbolic regression and hybrid expert ideas, the model parameters are fitted in partitions to construct a non-equilibrium factor correction model, which is then embedded into the CFD engineering code.
It achieves high-precision, physically interpretable, and computationally efficient non-equilibrium factor correction, improving the accuracy and efficiency of hypersonic flow field simulation.
Smart Images

Figure CN121996896B_ABST