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Design Parametric Study of a Compound Wing-in-Ground Effect. II: Aerodynamics Coefficients

机译:复合接地翼效应的设计参数研究。 II:空气动力学系数

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The aerodynamic behavior of the wing-in-ground effect can be affected by its configuration. This configuration is potentially the most influential parameter for the performance and stability of the wing-in-ground effect craft. As a continuation to the authors' previous works, in this research, the aerodynamic coefficients of the compound wing have been numerically investigated through the design parametric study in ground effect. The aerodynamics performances of the compound wing have been computed and the effects of various design parameters on the lift-to-drag ratio have been discussed in the previous paper. First, this paper validates the prediction method by comparing the lift coefficient of a rectangular wing with NACA 6409 airfoil for different angles of attack with an aspect ratio of 1.25 and ground clearance of 0.15. Then, the aerodynamic coefficients of the compound wing are computed over a range of various design parameters. As expected, all design parameters have effects on the aerodynamic coefficients. However, the effects of design parameters on the aerodynamic behavior of the compound wing are not equal. It was found that the span of the side wing, anhedral angle, and ground clearance have considerable effects on the ram effect pressure and the tip vortex of the compound wing. (C) 2015 American Society of Civil Engineers.
机译:机翼地面效应的空气动力学行为会受到其配置的影响。这种配置可能是对地面机翼效果飞行器的性能和稳定性影响最大的参数。作为作者先前工作的延续,本研究通过地面效应的设计参数研究对复合机翼的空气动力系数进行了数值研究。计算了复合机翼的空气动力性能,并在先前的论文中讨论了各种设计参数对升力比的影响。首先,本文通过比较直角比为1.25,离地间隙为0.15的NACA 6409翼型的矩形机翼在不同迎角下的升力系数,验证了预测方法。然后,在各种设计参数的范围内计算复合机翼的空气动力系数。正如预期的那样,所有设计参数都会对空气动力学系数产生影响。但是,设计参数对复式机翼空气动力学性能的影响并不相同。结果发现,侧翼的跨度,反角和离地间隙对撞角压力和复合翼的尖端涡流有相当大的影响。 (C)2015年美国土木工程师学会。

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