摘要
The numerical simulation prediction of aero-icing ice shape is usually complicated and time-consuming. In order to predict ice shape more quickly and accurately and to reduce computational resource consumption, a quick ice shape prediction method based on proper orthogonal decomposition and Kriging model is proposed in this paper. Using a database of high-fidelity CFD numerical simulations to build sample space, in view of the change of attack angle, the procedure for predicting the ice shape by reduced order model is introduced. With the data sampling method of parameter space, multiparameter prediction of the ice shape is achieved. Meanwhile, the related methods of the advanced Blind-Kriging model and the improvement of the prediction results are studied. The result shows that the prediction results of the airfoil icing shape using the reduced order model agree well with the CFD numerical simulation results. The conclusion is made that the reduced order model is a quick and accurate approach for predicting the ice shapes of airfoil icing.
投稿的翻译标题 | Ice shape prediction method of aero-icing based on reduced order model |
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源语言 | 繁体中文 |
页(从-至) | 1033-1041 |
页数 | 9 |
期刊 | Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics |
卷 | 45 |
期 | 5 |
DOI | |
出版状态 | 已出版 - 5月 2019 |
关键词
- Blind-Kriging model
- Ice-shape prediction
- Kriging model
- Proper orthogonal decomposition (POD)
- Reduced order model