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CFD Investigation of Flow Past Idealized Engine Nacelle Clutter

机译:氟氯烃综合发动机机舱杂乱的研究

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This research modeled low-speed flow past idealized engine nacelle clutter in support of aircraft fire suppression research. The idealized clutter was comprised of three vertical rows of staggered circular cylinders approximating typical nacelle obstructions such as fuel lines and wire bundles. Single-phase Detached-Eddy Simulations (DES) were conducted using the commercial CFD solver, Fluent?, to resolve the flow-field dynamics inside the clutter element. The goal of the simulations was to examine potential droplet transport and trapping mechanisms in the flow field which might inhibit or facilitate fire suppressant transport through engine clutter under low-speed flow conditions (ReD = 1, 575). The resulting numerical models provided no evidence that span-wise vorticity or three-dimensional shedding effects were responsible for transporting or trapping dispersed-phase particles. However, the simulations did demonstrate that suppressant droplets would likely follow a path governed by the vector sum of the local carrier fluid velocity and the velocity imposed by gravity. The Stokes number was computed from time-accurate data to determine the ability of dispersed particles to negotiate the clutter element without impinging on a cylinder. For slower free-stream velocities, Uoo = 1 rn/s, suppressant droplets (D = 90 /im) will likely be entrained in vortices shed from the intermediate row of cylinders and subsequently deposited on the last row of cylinders as the Karrnan vortex directly collides with the clutter. At free-stream velocities, Ux, = 5 m/s, the droplet particles will likely fail to track the carrier fluid streamlines in the cylinder wake and remain free of any shed vortices. Thus, the suppressant will conceivably transit the cylinder array without impact. These findings imply that a bluff-body turbulent diffusion flame in a cylinder wake could be nearly impossible to extinguish under high-speed, co-flow conditions. Conversely, suppressant transported by low-speed co-flow would experience difficulty traversing the cylinder array and reaching a downstream fire.
机译:这项研究模型低速流动过去的理想发动机机舱杂乱,支持飞机防火研究。理想化的杂波由三个垂直行的交错圆柱组成,近似典型的机舱障碍物,例如燃料管线和线束。使用商业CFD求解器进行单相分离涡流模拟(DES),流畅的?,以解决杂波元件内的流场动态。模拟的目标是检查流动场中的潜在液滴传输和捕获机制,这可能在低速流动条件下通过发动机杂波抑制或促进火灾抑制剂的捕获机制(Red = 1,575)。将得到的数值模型提供任何证据证明翼展方向涡或三维脱落效应负责运输或俘获分散的相颗粒。然而,模拟表明,抑制剂液滴可能遵循由局部载流体速度的矢量和管道管道的路径和重力施加的速度。从时准确的数据计算斯托克斯号以确定分散的颗粒在不撞击圆筒的情况下进行杂波元件的能力。对于较慢的自由流速度,UOO = 1 RN / S,抑制剂液滴(D = 90 / IM)可能会被夹带在圆柱体的中间行棚中,随后沉积在最后一排圆柱体上,直接karrnan vortex与杂乱碰撞。在自由流速度下,UX,= 5米/秒,液滴颗粒可能无法跟踪气缸醒来的载体流体流动线,并保持不含任何棚涡流。因此,抑制剂将可以想象地在没有冲击的情况下传输汽缸阵列。这些发现意味着汽缸唤醒中的虚张风湍流扩散火焰几乎不可能在高速,循环条件下熄灭。相反,低速混合运输的抑制剂将经历难以穿越气缸阵列并达到下游火灾。

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