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HELICOPTER ROTOR WAKE: STROBED LASER-SHEET VISUALIZATION

机译:直升机转子苏醒:频闪的激光片可视化

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The individual wakes trailing behind each blade of a helicopter rotor form turbulent vortex sheets that quickly roll into concentrated tip vortex filaments. A phase-locked, strobed laser light-sheet illuminating a seeded flow has been shown to provide both a quantitative and qualitative method to study the evolution of this turbulent wake. The tip vortex cores can be identified by a well-defined seed void. The shear layer produced by the blade wake appears as a line of discontinuity in the streaklines. Because the vortex core is a rolled-up portion of the original trailed wake, the vortex core and the vortex sheet were studied as interdependent flow structures. Some outboard portions of the vortex sheet were found to descend axially through the flow at a greater rate than the tip vortex core. While maintaining some connection to the original vortex core, the vortex sheet interacts with the tip vortex trailed from another blade. During the interaction, three-component laser Doppler velocimetry (LDV) measurements show a substantial increase in the angular velocity of the fluid within the vortex core. A three-dimensional reconstruction of the wake geometry in terms of the core trajectories agrees with results measured by LDV.
机译:尾波在直升机旋翼的每个叶片后面尾随,形成湍流的涡流片,迅速卷成浓密的涡旋丝。已经证明,照亮种子流的锁相,频闪激光片可提供定量和定性的方法来研究这种湍流尾流的演变。尖端涡流核可通过定义明确的种子空隙来识别。叶片尾流产生的剪切层在条痕线上表现为间断线。由于涡流芯是原始尾流的卷起部分,因此研究了涡流芯和涡流片作为相互依赖的流动结构。发现涡流片的一些外侧部分以比尖端涡流芯更大的速率轴向地通过流下降。在保持与原始涡旋核的某种连接的同时,涡旋片与从另一个叶片拖曳的尖端涡旋相互作用。在相互作用过程中,三分量激光多普勒测速(LDV)测量显示出涡旋核心内流体的角速度显着增加。在核心轨迹方面对尾流几何形状的三维重建与LDV测量的结果一致。

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    Department of Aerospace Engineering, Glenn L. Martin Institute of Technology, University of Mary, College Park, Maryland 20742;

    Department of Aerospace Engineering, Glenn L. Martin Institute of Technology, University of Mary, College Park, Maryland 20742;

    Department of Aerospace Engineering, Glenn L. Martin Institute of Technology, University of Mary, College Park, Maryland 20742;

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