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5. Experimental and Numerical Study on Composite Honeycomb Sandwich Paneles Subjected to Gelatime Bird

Experimental and Numerical Study on Composite Honeycomb Sandwich Paneles Subjected to Gelatime Bird

来源 :2nd International Conference on Lmpact Loading of Structural | 被引量 : 0次 | 上传用户：jinyu1016

【摘 要】

：

　　The composite honeycomb sandwich panel with two different sizes of 660mm×660mm×10.5mm and 660mm×660mm×5.5mm was designed.The thickness of honeycomb core

【作 者】

：

HUO Yujia XIE Jiang PEI Hui FENG Zhenyu 

【机 构】

：

TianjinKeyLaboratoryofCivilAircraftAirworthinessandMaintenance,CivilAviationUniversityofChina,Tianji

【出 处】

：

2nd International Conference on Lmpact Loading of Structural

【发表日期】

：

2018年5期

【关键词】

：

bird impact composite honeycomb sandwich dynamic response he layup angle 

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　　The composite honeycomb sandwich panel with two different sizes of 660mm×660mm×10.5mm and 660mm×660mm×5.5mm was designed.The thickness of honeycomb core is 10mm and 5mm respectively,the thickness of the composite laminate is 0.5 mm.

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