IMECH-IR  > 高温气体动力学国家重点实验室
A Fast Mathematical Modeling Method for Aerodynamic-Heating Predictions
Luo ZT(罗长童); Jiang ZL(姜宗林)
Source Publication31st International Symposium on Shock Waves 1
2019-03-22
Pages497-502
Conference Name31st International Symposium on Shock Waves
Conference Date2017-07-9~14
Conference PlaceNagoya, Japan
AbstractPrediction of aerodynamic heating under different flight conditions is a critical and challenging step in developing a new hypersonic vehicle. The prediction model usually involves a large number of variables, and this makes genetic programming converge too slow. This paper presents a fast mathematical modeling method, divide and conquer, for aerodynamic-heating predictions. It can use the separability feature of the target model to decompose a high-dimensional function into many low-dimensional sub-functions. The separability is detected by a special algorithm, bi-correlation test (BiCT), and the sub-functions could be determined by general genetic programming (GP) algorithms one by one. Thus the computational cost will be increased almost linearly with the increase of function dimension. This can help to break the curse of dimensionality and greatly improved the convergence speed to get the underlying target models from a set of sample data.
ISBN978-3-319-91020-8
Language英语
Document Type会议论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/80804
Collection高温气体动力学国家重点实验室
Recommended Citation
GB/T 7714
Luo ZT,Jiang ZL. A Fast Mathematical Modeling Method for Aerodynamic-Heating Predictions[C]31st International Symposium on Shock Waves 1,2019:497-502.
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