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Investigation of hydrodynamic lift & drag on an autonomous winged submarine using computational fluid dynamics

机译:利用计算流体力学研究自主翼型潜艇的水动力升力和阻力

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In the current study it has been analyzed the submarine take-off and subsequent submarine flight of a novel unmanned vehicle, has two operational modes: on sea surface as USV1 vehicle and submarine mode as UUV2.In the submarine mode the vehicle operates with the wings in a horizontal position and a specific speed that is needed for the immersion. The vehicle does not function as an underwater glider; it functions closer to an underwater aircraft. For that reason, the performance must be evaluated as a function of the generated "Drag" and "Lift". Due to the nature of its double purpose, it is required to know the performances in two conditions: fully submerged and on surface. These two cases will be analyzed with different numerical models for both scenarios, with free surface for USV mode and for the UUV mode. These scenarios are set out with four different numerical models which are: central body with central wing, central wing, central wing with flaps at 20 degrees and wing on surface. To measure the correlation between generated lift and speed a 1:2 scale model was used and tested in open waters. The data gathered in those tests was used to validate the mentioned CFD simulations.
机译:在目前的研究中,已经分析了一种新型无人飞行器的潜艇起飞和随后的潜艇飞行,该飞行器具有两种运行模式:在海面上为USV1运载工具,在水下模式为UUV2。在水平位置和浸入所需的特定速度。该车辆不能用作水下滑翔机;它的功能更接近水下飞机。因此,必须根据生成的“拖动”和“提升”来评估性能。由于其双重用途的性质,需要了解两种情况下的性能:完全浸入水中和表面上。对于这两种情况,将使用不同的数值模型来分析这两种情况,其中USV模式和UUV模式具有自由表面。这些情况通过四个不同的数值模型进行了阐述:带有中央机翼的中央机体,中央机翼,带20度襟翼的中央机翼和表面机翼。为了测量产生的升力和速度之间的相关性,使用了1:2比例模型并在开阔水域中进行了测试。这些测试中收集的数据用于验证上述CFD模拟。

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