In this thesis, the Canard Rotor/ Wing ( CRW) Aircraft is selected as the object of study. In response to the complicated characteristics of its flowfield, a CFD numerical simulation method for the CRW flowfield is established based on the momentum source model.

  • 以鸭式旋翼/机翼飞行器(CRW)为研究对象,针对CRW复杂流场结构的特点,建立了一套基于动量源模型的鸭式旋翼/机翼飞行器流场及气动特性的CFD分析方法。

  • 互联网摘选 2025-02-23 22:21:37

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