@inproceedings{4a09e4f9fd87492783fa49983ab7ecb7,
title = "RESEARCH OF PROPULSION-SYSTEM-SURROGATE-MODELING METHOD USING INFILL CRITERION SAMPLES",
abstract = "An accurate model of propulsion system is important to high altitude aircraft design. However, traditional approaches predicting propeller performance are often time-consuming. In this paper, a surrogate modeling method using infill criterion samples was chosen to refine the design process and reduce the time consumption. The results of this study show that the combination of infill criteria based surrogate model method and low-fidelity simulation can achieve comparable accuracy (average error of 5%) in prediction with the traditional approaches.",
keywords = "Design of experiments, High altitude aircraft propeller design, Infill criterion, Surrogate model",
author = "Dongchen Wang and Bifeng Song and Haifeng Wang and Jun Jiao",
note = "Publisher Copyright: {\textcopyright} 2021 32nd Congress of the International Council of the Aeronautical Sciences, ICAS 2021. All rights reserved.; 32nd Congress of the International Council of the Aeronautical Sciences, ICAS 2021 ; Conference date: 06-09-2021 Through 10-09-2021",
year = "2021",
language = "英语",
series = "32nd Congress of the International Council of the Aeronautical Sciences, ICAS 2021",
publisher = "International Council of the Aeronautical Sciences",
booktitle = "32nd Congress of the International Council of the Aeronautical Sciences, ICAS 2021",
}