Study on virtual test technology of liquid propellant engine

Na Duan; Li Hui Zhang; Shan Shan Xu; Zi Huan Zhu; Hai Lei Yu

Study on virtual test technology of liquid propellant engine

Na Duan^*
, Li Hui Zhang
, Shan Shan Xu
, Zi Huan Zhu
, Hai Lei Yu

^*此作品的通讯作者

宇航学院

Beihang University
China Aerospace Science and Technology Corporation

科研成果: 期刊稿件 › 文章 › 同行评审

摘要

The framework of the virtual test bed was designed. Objective/relationship mapping storage structure database system was developed, and the implementation flow of test management was analyzed. The development process of modeling and simulation module and virtual environment module was mainly explained. Then, the unique collaborative computing environment was developed via various interfaces, and the examples were given. At last, the advantages of applying virtual test in liquid rocket engine were concluded.

源语言	英语
页（从-至）	1659-1663
页数	5
期刊	Hangkong Dongli Xuebao/Journal of Aerospace Power
卷	25
期	7
出版状态	已出版 - 7月 2010

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引用此

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title = "Study on virtual test technology of liquid propellant engine",

abstract = "The framework of the virtual test bed was designed. Objective/relationship mapping storage structure database system was developed, and the implementation flow of test management was analyzed. The development process of modeling and simulation module and virtual environment module was mainly explained. Then, the unique collaborative computing environment was developed via various interfaces, and the examples were given. At last, the advantages of applying virtual test in liquid rocket engine were concluded.",

keywords = "Engineering database, Hierarchical structure, Liquid rocket engine, Oriented object, Virtual experiment",

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N2 - The framework of the virtual test bed was designed. Objective/relationship mapping storage structure database system was developed, and the implementation flow of test management was analyzed. The development process of modeling and simulation module and virtual environment module was mainly explained. Then, the unique collaborative computing environment was developed via various interfaces, and the examples were given. At last, the advantages of applying virtual test in liquid rocket engine were concluded.

AB - The framework of the virtual test bed was designed. Objective/relationship mapping storage structure database system was developed, and the implementation flow of test management was analyzed. The development process of modeling and simulation module and virtual environment module was mainly explained. Then, the unique collaborative computing environment was developed via various interfaces, and the examples were given. At last, the advantages of applying virtual test in liquid rocket engine were concluded.

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KW - Hierarchical structure

KW - Liquid rocket engine

KW - Oriented object

KW - Virtual experiment

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SN - 1000-8055

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JO - Hangkong Dongli Xuebao/Journal of Aerospace Power

JF - Hangkong Dongli Xuebao/Journal of Aerospace Power

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Study on virtual test technology of liquid propellant engine

摘要

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