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Reynolds-Averaged Navier-Stokes Simulations of Helicopter Slung Loads

机译:雷诺直升机惯性载荷的平均Navier-Stokes模拟

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This paper summarizes a body of work that focuses upon the aerodynamics of slung load containers. Two different computational fluid dynamics Reynolds- Averaged Navier-Stokes codes, OVERFLOW-D and Star- CD, were used to study flows over bluff bodies representative of bluff bodies. These studies include twodimensional flows across square shapes and cross-section of the Container Express (CONEX), and of threedimensional flows across cubes and of the CONEX. These highly unsteady flow fields were performed for static bodies, bodies undergoing spin, and bodies undergoing forced oscillations. The computations demonstrate a capability in predicting both static and moving body computations using these two different CFD methods. The computed results highlight some of the requirements for obtaining useful solutions and also give some insight into the complicated aerodynamics associated with theseconfigurations.
机译:本文总结了一项工作,重点是悬吊式装载容器的空气动力学。使用两种不同的计算流体动力学雷诺平均Navier-Stokes码OVERFLOW-D和Star-CD来研究代表阻流体的阻流体上的流动。这些研究包括跨容器Express(CONEX)的正方形形状和横截面的二维流,以及跨立方体和CONEX的三维流。这些高度不稳定的流场是针对静态物体,经历自旋的物体和经历强制振荡的物体进行的。这些计算展示了使用这两种不同的CFD方法预测静态和运动体计算的能力。计算结果突显了获得有用解决方案的一些要求,并且也使您对与这些配置相关的复杂空气动力学有了一定的了解。

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