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基于流程图的飞机液冷系统组态建模及仿真
引用本文:南国鹏,王浚.基于流程图的飞机液冷系统组态建模及仿真[J].系统仿真学报,2004,16(4):714-716,744.
作者姓名:南国鹏  王浚
作者单位:北京航空航天大学飞行器设计与应用力学系,北京,100083
摘    要:结合国内某飞机液冷系统的研制,利用热动力理论建立了系统主要组件的数学模型,同时采用面向对象的编程思想,在VC 6.0软件开发平台上,自行编制了基于流程图的液冷系统组态图形仿真软件(LCS-1.0)。该软件弥补了地面试验条件的不足,为液冷系统稳、动态性能分析提供了方便、快捷的实现途径。算例针对国内某飞机液冷系统进行了性能分析,计算值与试验值吻合良好。

关 键 词:飞机  液体冷却  组态建模  动态仿真
文章编号:1004-731X(2004)04-0714-03

Configuration Modeling and Simulation of Aircraft Liquid Cooling System Based on Flow Chart
NAN Guo-peng,WANG Jun.Configuration Modeling and Simulation of Aircraft Liquid Cooling System Based on Flow Chart[J].Journal of System Simulation,2004,16(4):714-716,744.
Authors:NAN Guo-peng  WANG Jun
Abstract:Base on the research of the Liquid Cooling System (LCS) of one domestic fighter, mathematical models of the main components are set up with the thermodynamics theory. Meanwhile, a configuration graphics simulation software (LCS-1.0) of LCS based on the flow chart has been developed with the object-oriented program concept on VC 6.0 Integrated Developing Platform (IDP). It makes up the disadvantages of ground test conditions and facilitates the analysis of steady and dynamic performance of LCS. An example analyses the performance of LCS of a certain fighter in our country, and the calculated values are in consistent with the test results.
Keywords:aircraft  liquid cooling  configuration modeling  dynamic simulation
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