@inproceedings{54d4f988a9b3442bafec9a5f19f7827c,
title = "Modeling of the boom refueling system and simulation analysis of pressure shock peculiarity of the fuel receptacle",
abstract = "There is intense pressure shock in the boom refueling system because of the fuel receptacle shutting down suddenly and the fuel flow decreasing to zero soon when the refueling process finished, which the aerial refueling system even flight security will be damaged. In this paper, the software, AMESim will be applied to establish the model of the boom refueling system of a certain type of aircraft, and the influence on the system pressure shock of the fuel receptacle is analyzed in two aspects: The closing time and the close curve.",
keywords = "Aerial refueling, Boom, Fuel receptacle, Pressure shock, Simulation",
author = "Xiaogang Li and Zhou Zhou and Yonglin Li and Keqiang Cao",
note = "Publisher Copyright: {\textcopyright} 2017 IEEE.; 2017 International Conference on Sensing, Diagnostics, Prognostics, and Control, SDPC 2017 ; Conference date: 16-08-2017 Through 18-08-2017",
year = "2017",
month = dec,
day = "9",
doi = "10.1109/SDPC.2017.49",
language = "英语",
series = "Proceedings - 2017 International Conference on Sensing, Diagnostics, Prognostics, and Control, SDPC 2017",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
pages = "220--225",
editor = "Wei Guo and {de Oliveira}, {Jose Valente} and Chuan Li and Yun Bai and Ping Ding and Juanjuan Shi",
booktitle = "Proceedings - 2017 International Conference on Sensing, Diagnostics, Prognostics, and Control, SDPC 2017",
}