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	Aero engine numerical simulation platform based on VC++ language
	Wu Yu ; Yu Long-jiang ; Piao Ying
	2010-10-12 ; 2010-10-12
关键词	Practical/ aerospace computing aerospace engines aerospace simulation C++ language user interfaces/ aero engine numerical simulation platform VC++ language digital engine controller aero-thermodynamic models user interface/ B7620 Aerospace testing and simulation B7640 Aerospace propulsion C7460 Aerospace engineering computing C6110J Object-oriented programming C6180 User interfaces
中文摘要	In order to fulfill the semi-physical test of a digital engine controller, this paper develops aero-thermodynamic models of the engine's components using VC++ language according to the engine's aerodynamic arrangement, the geometry and the component's test characteristics. Thorough consideration is given to the independency of each component and the interaction of aero-thermodynamic parameters of flow-path components in process of constructing classes, to the extent that the component model can represent the real status of the engine working in transient process calculation as well as can be easily connected. Friendly user interface is developed. The simulation results show that the platform has good efficiency and precision.
语种	中文
出版者	Editorial Board of Computer Engineering ; China
内容类型	期刊论文
源URL	[http://hdl.handle.net/123456789/78960]
专题	清华大学
推荐引用方式 GB/T 7714	Wu Yu,Yu Long-jiang,Piao Ying. Aero engine numerical simulation platform based on VC++ language[J],2010, 2010.
APA	Wu Yu,Yu Long-jiang,&Piao Ying.(2010).Aero engine numerical simulation platform based on VC++ language..
MLA	Wu Yu,et al."Aero engine numerical simulation platform based on VC++ language".(2010).

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