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Numerical Simulation of Helicopter Ditching on Wavy Water

机译:直升机在水面上开沟的数值模拟

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The present study explored the ditching characteristics of a three-dimensional helicopter model on wavy water, where the effects of water-entry wave positions, including crest, falling, rising and trough wave were assessed by means of numerical simulation. The air-water two phase flow is computed by solving unsteady Reynolds-Averaged Navier-Stokes equations enclosed by standard k-omega turbulence model. The volume of fluid model is applied for the sake of capturing the air-water interface. The relative motion between the helicopter and water is treated by a global moving mesh method. Results show the effects of wave positions and initial pitching angles on the ditching event in detail. It is observed that crest and falling wave are the optimal choices when the helicopter makes a ditching event on wavy water. Furthermore, an optimal pitching angle at 6 deg is obtained for the helicopter ditching case in this paper.
机译:本研究探索了三维直升机模型在波浪水上的排水特性,其中通过数值模拟评估了水波位置(包括波峰,下降,上升和波谷)的影响。通过求解标准k-ω湍流模型所包含的非稳态雷诺平均Navier-Stokes方程,可以计算出空气-水两相流。应用流体模型是为了捕获空气-水界面。直升机与水之间的相对运动通过整体移动网格方法进行处理。结果详细显示了波浪位置和初始俯仰角对俯冲事件的影响。可以看到,当直升机在波涛汹涌的水面上进行开沟事件时,波峰和落波是最佳选择。此外,本文针对直升飞机的俯仰情况获得了最佳的6度俯仰角。

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