摘要
通过先进气动外形缩比倾转旋翼的动力学设计,对倾转旋翼结构动力学设计中的特殊问题和重点问题形成了系统的研究,并提出了倾转旋翼结构动力学的工程设计准则和设计方法;基于该准则和方法设计的缩比倾转旋翼已用于风洞试验。
Important and special structure dynamic problem had systemic researched in a project which used 3 advanced geometry blades on a scaled tilt - rotor design. The design criteria of tilt - rotor structure dynamic had been presented. The scale rotor which followed the criteria had work in wind tunnel test.
出处
《直升机技术》
2017年第1期1-7,30,共8页
Helicopter Technique
基金
863计划"先进直升机技术"(2012AA112201)
