This paper introduces a method of making selection of helicoptertailrotor parameter optimization using computer optimum techniques.
本文介绍采用计算机优化技术进行直升机尾桨参数优化选择的方法。
2
In a helicopter the articulated head and tailrotor gearbox are required to be a very high specification design using the best materials and requiring frequent and costly maintenance.
在直升机的阐述头和尾桨变速箱都必须是一个非常高规格的设计使用最好的材料和需要频繁和昂贵的维修。
3
For the current helicopter of single main rotor with tailrotor, the effect of inflow models with different characteristics on helicopter trim and digital simulation was discussed.