Researchers worldwide quoted several concepts, in order to suppress or eliminate the undesired effect of dynamic stall.
国内外研究者为此提出了多种不同的控制方案,以期减轻或消除动态失速的负面影响。
参考来源 - 直升机旋翼前缘下垂控制动态失速数值模拟研究The dynamic stall model is based on the Beddoes-Leishman model which evolves from the helicopter theory.
动态失速模型以直升机理论的Beddoes-Leishman模型为基础。
参考来源 - 水平轴风力机动态气动问题研究及软件开发·2,447,543篇论文数据，部分数据来源于NoteExpress
The dynamic stall experiment is an unsteady aerodynamic test, whose experimental data are random.
动态失速风洞实验是一种非定常实验，其测量所得数据属于随机数据范畴。
Abstract: The dynamic stall experiment is an unsteady aerodynamic test, whose experimental data are random.
文摘：动态失速风洞实验是一种非定常实验，其测量所得数据属于随机数据范畴。
This paper includes four sections: aerodynamic analysis and calculation, turbulent wind field model, dynamic stall model, develop software with COM.
论文包括四部分：气动分析与计算理论、紊流风场模型、动态失速模型、组件软件开发。
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