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高位垂直进气转静系旋转盘腔流场的实验
引用本文:陶智,高娟,蔡毅,丁水汀,罗翔,邹正平.高位垂直进气转静系旋转盘腔流场的实验[J].航空动力学报,2007,22(3):347-351.
作者姓名:陶智  高娟  蔡毅  丁水汀  罗翔  邹正平
作者单位:北京航空航天大学,能源与动力工程学院,航空发动机气动热力重点实验室,北京,100083;西安航空发动机(集团)有限公司,西安,710021
摘    要:利用粒子图像测速技术(简称PIV)对高位垂直进气的转静系旋转盘腔流场进行了实验研究.该盘腔由一个旋转盘、一个静止盘及静止的外围盘罩组成.实验结果表明:PIV粒子成像技术可以应用于旋转盘腔结构的流场测试, 在本实验的工况范围内, 大部分区域的流动已为湍流, 两盘间的流动结构明显具有Batch-elor流型的特点, 转盘和静盘两个表面附近形成各自独立的边界层, 两边界层之间有一个旋转核心, 核心区内旋流系数β比大间隙封闭系统湍流流动时旋流系数的值0.43要小.流量系数和旋转雷诺数的变化对旋流系数β的影响较小, 但转静间隙的变化对β的影响较为显著. 

关 键 词:航空、航天推进系统  转静系  旋转盘腔  PIV  流场  旋流系数
文章编号:1000-8055(2007)03-0347-05
收稿时间:2006/3/27 0:00:00
修稿时间:2006年3月27日

Experimental investigation of the flow field between a rotating and a stationary disk at high-positioned air inflow
TAO Zhi,GAO Juan,CAI Yi,DING Shui-ting,LUO Xiang and ZOU Zheng-ping.Experimental investigation of the flow field between a rotating and a stationary disk at high-positioned air inflow[J].Journal of Aerospace Power,2007,22(3):347-351.
Authors:TAO Zhi  GAO Juan  CAI Yi  DING Shui-ting  LUO Xiang and ZOU Zheng-ping
Institution:1.National Key Laboratory on Aero-Engines, School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, Beijing 100083, China2.Xi'an Aero-Engine(GROUP) LTD, Xi'an 710021, China
Abstract:The flow field between a rotating and a stationary disk at high-positioned air inflow condition was investigated by Particle Image Velocimetry(PIV) technology.The experiments indicate that PIV technology could be used on the flow measurement of the rotating cavity.The flow in the most area became turbulence in the range of experiments.Batchelor-type flow was observed in the experiments.Separate boundary layers were formed on the rotor and stator.Between the boundary layers there was an inviscid core rotating in the same direction as the rotor at a lower speed.The experimental data of the relative rotational speed β in the core was lower than 0.43,the value in the closure system with large clearance.β did not show obvious changes with the change of flow rate coefficient or rotational Reynolds number,but the axial clearance between the rotor and stator affected β much obviously. 
Keywords:aerospace propulsion system  rotating-stationary-disk system  rotating cavity  Particle Image Velocimetry(PIV)  flow field  relative rotational speed
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