model rotor meaning in Chinese

模型转子

Their availability , stability , and robustness are proved by simulation on both model rotor and real rotor with the effect of the design parameters of the flap studied
对模型与真实旋翼进行仿真计算并研究后缘附翼设计参数的影响，结果表明两种方法都具有较好的有效性、稳定性和鲁棒性。
In chapter 5 , the uh - 1 model rotor , the model rotor measured in the present work and the helicopter z - 8 rotor are taken as numerical examples , the calculations on rotor noise under different flight conditions are carried out for validation purposes
应用该模型，分别以uh - 1模型旋翼、本文试验的模型旋翼以及z - 8直升机旋翼为算例，对不同飞行条件下的旋翼气动噪声进行了计算，验证了本文的计算方法。