摘要
阐述了将结构热试验和气动加热计算相结合,实现气动热分析与热试验相耦合的试验控制方法。为飞行器的气动加热和结构热响应耦合分析提供了一个解决思路,同时为结构热试验热载荷条件的制定提出了新的方法,对应用复杂防热结构的飞行器的气动热分析和结构热试验具有重要的意义。
Based on thermo-structural experiment, coupling of aeroheating analysis and thermal test, a new experimental control method is described. It applies a new method for coupling analysis of aeroheating and thermal response, and for instituting heating load conditions of thermo-structural experiment. This method is important to aero-heating analysis and thermo-structural experiment for any aerocraft with duplicate heat insulation structures.
出处
《强度与环境》
2006年第4期59-63,共5页
Structure & Environment Engineering
关键词
气动热分析
结构热试验
耦合
飞行器
aeroheating analysis： thermo-structural expedment
coupling
