试验表明，该系统可用于复合材料结构和蜂窝夹层结构的无损检测。
It is concluded that the system can be used in nondestructive detection of composite material and honeycomb structure.
蜂窝夹层结构已成为雷达罩结构设计中广泛应用的重要材料。
Honeycomb sandwich has become an important material in designing radomes instruction.
飞机复合材料零件结构分为蜂窝结构、夹心结构、空心结构、夹层结构等。
Structures of aircraft composite parts include honeycomb, inner contained part, inner empty part, and layered etc.
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；
The in-plane and through-thickness direction temperature distribution of composite honeycomb sandwich structure repaired by hot bonder was tested with thermocouples.
试验证明，该系统可成功用于复合材料结构和蜂窝夹层结构的无损检测。
Experiment proved that the system was successful for the nondestructive testing of composite and honeycomb interlayer structures.
通过理论设计及CAD辅助计算得到了一种“陷阱”式的宽频带层板型结构吸波材料和一种宽频带蜂窝夹层型结构吸波材料。
By theoretical design and CAD, a kind of wide frequency-width Radar Absorbent Structure Plate named "trap" and a kind of wide frequency-width Radar Absorbent Honeycomb Sandwich Material are obtained.
本文对碳纤维复合材料蜂窝夹层结构侧压强度进行了理论计算，试验值在理论计算范围内。
Theoretical calculation of edge Compressio strength of CFRP Sanduich Construction with honey core is gotten in this paper. The test value is in the range of theoretical Caculation.
本文对碳纤维复合材料蜂窝夹层结构侧压强度进行了理论计算，试验值在理论计算范围内。
Theoretical calculation of edge Compressio strength of CFRP Sanduich Construction with honey core is gotten in this paper. The test value is in the range of theoretical Caculation.
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