高速飞行器热结构力热参数先进测试技术概述  

Overview of Advanced Testing Technologies for Mechanical and Thermal

作　　者：王晓晖[1] 王智勇[1] 宫文然[1] 王则力[1] 王成亮[1] 武小峰 WANG Xiaohui;WANG Zhiyong;GONG Wenran;WANG Zei;WANG Chengiang;WU Xiaofeng(Beijing Institute of Structure and Environment Engineering,Beijing 100076,China)

机构地区：[1]北京强度环境研究所,北京100076

出　　处：《强度与环境》2023年第6期97-107,共11页Structure & Environment Engineering

基　　金：国家自然科学基金联合基金项目(U20B2002);自然科学基金青年基金项目(11802033)。

摘　　要：地面试验中准确的力热载荷和结构响应参数的获取,是考核和评价飞行器结构性能的依据和条件。本文针对高速飞行器热结构试验中常用的力热参数测试技术,介绍了相关原理及试验应用中需解决的问题,指出了未来的发展方向。通过上述研究,以期为相关工程技术人员提供参考,推动高速飞行器力热参数测试技术领域向着更高水平发展。The accurate acquisition of mechanical-thermal loads and structural response parameters in ground tests is the basis and condition for assessing and evaluating the structural performance of aircraft.This airticle focuses on the commonly used mechanical-thermal parameter testing technologies in the high-temperature structure testing of high-speed aircraft,introduces relevant principles and the problems that need to be solved in the testing application,and points out the future development direction.Through above research,we hope to provide reference for relevant engineers,and promote the development of mechanical-thermal parameter testing technologies for high-speed aircraft.

关 键 词：高速飞行器 热结构 光纤应变 光测技术 

分 类 号：V416.4[航空宇航科学与技术—航空宇航推进理论与工程] TJ06[兵器科学与技术—兵器发射理论与技术] O348.5[理学—固体力学]