aeromechanical meaning in Chinese

航空力学的

As one of the basic problem of helicopter dynamics , the aeromechanical stability of the coupled rotor - body system has been paid a lot of attention
直升机旋翼/机体耦合系统的气动机械动稳定性问题是直升机动力学的基本问题之一,长期以来一直受到人们的普遍关注。
In order to analyze this model , a modified multi - blade coordinate transformation was proposed . at last , the aeromechanical stability problem was analyzed with the two
最后用上述两种分析方法对带叶间减摆器的旋翼/机体耦合系统的气动机械稳定性问题进行了分析研究。
To study the influence of this damper configuration to aeromechanical stability , some work has been done in this thesis . first , dynamic equation of the rotor - hub system was modeled with the generalized hamilton principle , which can be used to analyze the stability problem in different conditions like on - ground , hovering and flight . when fastening the fuselage , the model can also be used to analyze the stability problem of isolated rotor system
为了研究这种新型布置减摆器对直升机稳定性的影响,本文所作研究工作如下:首先,本文利用广义的hamilton原理建立了适用于不同状态(地面、悬停和前飞)的旋翼/机体耦合系统的动力学模型,该模型中将机体固定可以用来分析孤立旋翼的稳定性问题。