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Influence of the Pappus Shape of Bionic dandelion aircraft on Drag Characteristics

机译:仿生蒲公英飞机Pappus形状对拖曳特性的影响

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This paper mainly reveals the inherent mechanism how dandelion pappus shape affects the formation of stable separated vortex ring (SVR) and the flight drag characteristics of bionic dandelion aircraft. Firstly, based on the morphometric results of super dandelion seeds and dandelion seeds, the geometric model of bionic dandelion aircraft was established. Secondly, the computational fluid dynamics (CFD) simulation of a single cylindrical pappus, a cuboid pappus and bionic aircraft models with cylindrical or cuboid pappi is carried out. Finally, the simulation results are analyzed and compared with the relevant experimental results. The results proves that the porosity of bionic dandelion aircraft is not the absolute factor to determine the drag coefficient, and the pappus shape is also an important factor which should be considered in the design of bionic dandelion aircraft. The results of this paper can explain how the pappus shape affects the formation of stable SVR and the drag coefficient, which is of great significance for the design of bionic dandelion aircraft.
机译:本文主要揭示了固有机制蒲公英Pappus形状如何影响稳定分离的涡旋环(SVR)的形成以及仿生蒲公英飞机的飞行阻力特性。首先,基于超蒲公英种子和蒲公英种子的形态测量结果,建立了仿生蒲公英飞机的几何模型。其次,进行单个圆柱形PAPPUS的计算流体动力学(CFD)模拟,具有圆柱形或长方体Pappi的长方体PAPPUS和仿生飞机模型。最后,分析了模拟结果并与相关实验结果进行了比较。结果证明,仿生蒲公英飞机的孔隙率不是确定拖曳系数的绝对因素,并且Pappus形状也是在仿生蒲公英飞机设计中应考虑的重要因素。本文的结果可以解释PAPPUS形状如何影响稳定的SVR和拖曳系数的形成,这对于仿生蒲公英飞机的设计具有重要意义。

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