the mechanical properties of a kind of honeycomb sandwich structure with the face of carbon fiber composites and aluminum honeycomb under particle radiation, ultraviolet ray are measured.
the in-plane and through-thickness direction temperature distribution of composite honeycomb sandwich structure repaired by hot bonder was tested with thermocouples.
利用热电偶测试热补仪修补复合材料蜂窝夹层结构的面内及厚度方向的温度分布;
to identify the dynamic characteristic of honeycomb sandwich structure via method mentioned in this thesis can be valuable in practice for further design.