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首页> 外文期刊>Chinese journal of aeronautics >Prediction of Aerodynamic Interaction of helicopter Rotor on its Fuselage
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Prediction of Aerodynamic Interaction of helicopter Rotor on its Fuselage

机译:直升机旋翼机体气动相互作用的预测

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摘要

An iterative and full-coupled rotor/fuselage aerodynamic interaction analytical method is developed based upon the rotor free-wake model and the 3-D fuselage panel model. A close vortex/ surface interaction model using the Analytical/Numerical Matching (ANM) was adopted in the method in order to simulate effectively the unsteady close interaction between the rotor tip-vortex and fuselage surface. By the analytical method, the unsteady and steady pressure distribution on the fuse- lage surface, and the unsteady lift and pitching moment of the fuselage in a rotor interaction environ- ment were calculated for different advance ratios.
机译:基于转子自由尾迹模型和3-D机身面板模型,提出了一种迭代的全耦合式转子/机身气动相互作用分析方法。该方法采用了一种利用解析/数值匹配(ANM)的紧密涡/表面相互作用模型,以便有效地模拟转子尖端涡流与机身表面之间的非稳态紧密相互作用。通过分析方法,可以计算出在不同的推进比情况下,在转子相互作用环境下,机身表面的非稳态压力和稳态压力分布,以及机身的非稳态升力和俯仰力矩。

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