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Experimental Investigation of a Wing-in-Ground Effect Craft

机译:机翼效应飞机的实验研究

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摘要

The aerodynamic characteristics of the wing-in-ground effect (WIG) craft model that has a noble configuration of a compound wing was experimentally investigated and Universiti Teknologi Malaysia (UTM) wind tunnel with and without endplates. Lift and drag forces, pitching moment coefficients, and the centre of pressure were measured with respect to the ground clearance and the wing angle of attack. The ground effect and the existence of the endplates increase the wing lift-to-drag ratio at low ground clearance. The results of this research work show new proposed design of the WIG craft with compound wing and endplates, which can clearly increase the aerodynamic efficiency without compromising the longitudinal stability. The use of WIG craft is representing an ambitious technology that will help in reducing time, effort, and money of the conventional marine transportation in the future.
机译:通过实验研究了具有复合机翼高贵构型的机翼地面效应(WIG)工艺模型的空气动力学特性,并使用了有无端板的马来西亚科技大学(UTM)风洞。相对于离地间隙和机翼迎角,测量了升力和阻力,俯仰力矩系数和压力中心。地面效应和端板的存在增加了低离地间隙时机翼的升阻比。这项研究的结果表明,采用复合机翼和端板的WIG飞机的新设计方案可以明显提高空气动力学效率,而不会损害纵向稳定性。 WIG工艺的使用代表着一项雄心勃勃的技术,它将有助于减少传统海上运输的时间,精力和金钱。

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