摘要
本文将经典的直升机桨叶强度分析方法推广到更加符合实际情况的模糊可靠性分析上去。本文算例说明它们之间的差异不可忽略。
In this paper,the classical strength analysis method for helicopter rotor blades is extended to fuzzy reliability analysis method which conforms to reality better.The numerical example in the paper shows that the difference between the results based on classical analysis and those predicted by reliability and fuzzy reliability analysis can not be neglected.
出处
《直升机技术》
1994年第3期29-31,共3页
Helicopter Technique
