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Experimental Investigation of the Ground Effect of WIG Craft—NEW1 Model

机译:WIG Craft-New1模型的实验研究

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Navy Experimental Wing-in-Ground-Effect (WIG) craft namely as NEW1, is the first version of 2-seated WIG craft which has been designed and developed by Royal Thai Navy since 2017. This experimental research is a part of the NEW1 project which aims to investigate the aerodynamic characteristics and aspects of the flow passing through the WIG craft model when in ground effect. In the experiment, the WIG craft—NEW1 of 1:15 scale model is tested in a close circuit wind tunnel of 1 m × 1 m test section at Kasetsart University. The tests are conducted at the free stream velocity of 40 m/s or Reynolds number of 280,000, at angles of attack ranging from −9° to 21°, and at the wing to ground distances ranging from 5.0 C to 0.3 C. The measurement of 6-DoF of forces and moments and pressure distributions on the ground surface underneath the WIG craft model are made during the tests. The results show that the ground has significant effects on the aerodynamic characteristics of the WIG craft model when the wing to ground distance is less than its mean chord. It was found that when the model move from 5.0 C (out of ground effect) to 0.3 C, the lift coefficient increases up to 15.7%, the drag coefficient decreases up to 5.6%, and the lift to drag ratio increases 33.4%. The proximity of the model to the ground also affects the longitudinal stability of the model. The moment coefficient curves against angle of attack has negative slope for both in and out of ground effect indicating favorable longitudinal stability. However, it was found that the aerodynamic center move further aft toward the trailing edge when the model move closer to the ground.
机译:海军实验翼型效果(WIG)艺术是新的1,是由2017年皇家泰国海军设计和开发的第一个版本的2座假发工艺版本。该实验研究是新的项目的一部分旨在调查通过在地面效果上通过假发工艺模型的流动的空气动力学特征和方面。在实验中,假发工艺和MDASH; 1:15比例模型的新增型在1米的近电路风隧道中进行了测试; Kasetsart大学1米测试部分。该试验以自由流速度为40米/秒或雷诺数为280,000,在攻击角度范围内的攻击范围和减去; 9&Deg;在21℃,并且在机翼以5.0c至0.3℃的距离范围为0.3℃。在测试期间,在假发工艺模型下面的地表上的6-DOF的测量和矩和压力分布的测量。结果表明,当机翼与地面距离小于其平均弦时,地面对假发工艺模型的空气动力学特性具有显着影响。结果发现,当模型从5.0℃移动到0.3℃时,升力系数增加高达15.7%,拖曳系数降低至5.6%,升力比率增加33.4%。模型对地面的接近也影响了模型的纵向稳定性。瞬间与攻角角度曲线具有负斜率,用于进出接地效果,表明纵向稳定性有利。然而,发现当模型移动到地面时,空气动力学中心进一步向后移动。

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