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fu he cai liao fei ji jie gou wan zheng xing qiang du yan zheng ji shu
Author(s): 
Pages: 32-38,63
Year: Issue:  1
Journal: AIRCRAFT DESIGN

Keyword:  复合材料结构完整性强度验证关键技术;
Abstract: 根据国军标<军用飞机结构完整性大纲--飞机要求>,结合研制复合材料机翼和复合材料垂直尾翼摸索出的成功经验,总结归纳出强度验证几项关键技术:如何解决疲劳分散性;如何修正载荷谱;如何选取试验项目;如何制定验证试验程序;如何人工预制冲击损伤;如何进行无损检测;"静力覆盖疲劳"与"损伤不扩展"结构设计必要条件是什么.
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