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Thermal damage analysis of aircraft composite laminate suffered from lightning swept stroke and arc propagation 被引量:4
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作者 Xiangteng MA Fusheng WANG +2 位作者 Han CHEN Donghong WANG Bin XU 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2020年第4期1242-1251,共10页
Lightning strike is a complicated process involving multi-field coupling.In order to investigate the thermal damage mechanism of carbon fiber reinforced composites subject to lightning swept stroke,a complete numerica... Lightning strike is a complicated process involving multi-field coupling.In order to investigate the thermal damage mechanism of carbon fiber reinforced composites subject to lightning swept stroke,a complete numerical method is presented.Numerical model of lightning discharge is established based on Magneto Hydro Dynamics(MHD)and calculated by FLUENT secondary development technology.Considering aerodynamic flow effect,channel formation and evolution process during lightning discharge is analyzed for lightning current waveform A.Thermal-electric Coupling model is presented according to Radial Basis Function(RBF)interpolation theory,which is implemented by compiling program to make lightning current and heat energy inject into composite laminate.Consequently,damage mechanism of composite laminate under lightning swept stroke is studied based on the coupled numerical model and element deletion method.Ablation damage morphology of composite laminate is analyzed to understand plasma expansion and reattachment in arc root.The results show that aerodynamic flow makes the lightning channel move fast and composite laminate is deteriorated due to thermal damage. 展开更多
关键词 Ablation damage Composite laminates Coupling data transfer Element deletion Lightning swept stroke
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H425直升机雷击分区 被引量:5
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作者 李继国 郎需义 《高电压技术》 EI CAS CSCD 北大核心 2017年第5期1420-1424,共5页
直升机雷击分区对其进行雷电防护设计具有重要指导意义。为此,分别以雷电试验和数值仿真2种方法对H425直升机展开雷击分区研究。运用FEKO软件计算了雷电电场环境下直升机机体表面电荷分布情况,模拟分析直升机的雷击附着区域分布,绘制了... 直升机雷击分区对其进行雷电防护设计具有重要指导意义。为此,分别以雷电试验和数值仿真2种方法对H425直升机展开雷击分区研究。运用FEKO软件计算了雷电电场环境下直升机机体表面电荷分布情况,模拟分析直升机的雷击附着区域分布,绘制了直升雷击附着区域分布图。采用4.8 MV冲击电压发生器,对直升机的缩比模型进行雷击附着点试验,并根据雷击附着点的统计,分析了直升机雷击可能附着的区域。通过雷击分区研究,给出了H425直升机雷击分区图,并对直升机水平安定面进行了更精确的分区。研究结果表明:带侧端板的水平安定面在侧端板底端附着雷电的概率较大,应将其划为雷击附着区;旋翼桨毂附着雷电概率小,应将其划为雷电扫掠区。研究结果对其它型号直升机的雷电防护设计具有借鉴意义。 展开更多
关键词 直升机 雷击分区 附着点 扫掠冲击 FEKO 缩比模型
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