吴志昌,王宝坤,李诗军,杨 嵩,杜长明,王志鹏.露天试车台侧风装置气动特性数值模拟[J].航空发动机,2024,50(4):150-155
露天试车台侧风装置气动特性数值模拟
Numerical Simulation of Outdoor Test Bed Crosswind Device Aerodynamic Characteristics
  
DOI:
中文关键词:  露天试车台  侧风装置  气动特性  数值模拟  航空发动机
英文关键词:outdoor test stand  crosswind device  aerodynamic characteristics  numerical simulation  aeroengine
基金项目:航空动力基础研究项目资助
作者单位
吴志昌,王宝坤,李诗军,杨 嵩,杜长明,王志鹏 中国航发沈阳发动机研究所沈阳 110015 
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中文摘要:
      为了探究露天试车台侧风装置的气动流场特性,采用商用软件构建了侧风装置的全3维数值模型,完成了侧风装置气 动特性的数值模拟。结果表明:安装在靠近侧风装置壁面附近的风机对风场边界产生影响,最中间1台风机排出的气流直接影响 速度核心区中心风场,临近最中间水平方向两侧的2台风机排出的气流对关注截面偏离z中心轴线±0.25D位置产生影响;气流从 侧风装置排出后可发现核心流速区、掺混区和低速扰动区3个区域,核心流速区内的气流变化平稳,未见大的波动;在以发动机进 气轴线为中心d=0.8D直径范围内,随着风速的增大,最大流速差逐渐增大,速度不均匀度逐渐减小。研究结果可为发动机开展侧 风试验提供理论和技术基础。
英文摘要:
      In order to explore the aerodynamic flow field characteristics of the crosswind device of an outdoor test bed, a full 3D numerical model of the crosswind device was constructed by using commercial software, and numerical simulations of the aerodynamic characteristics of the device were conducted. The results show that the fans installed near the wall of the crosswind device have an impact on the boundary of the wind field, The airflow discharged from the central fan directly affects the central wind field in the core region, and the airflow dischaged by the two fans on the horizontal center plane which reside on both sides and just next to the centerline has an impact on the positions deviating from the z axis by ± 0.25D on the interested cross-section (the cross-section that 1.695D away from the outlet of the crosswind device, where D is the outlet hydraulic diameter of the crosswind device). After the airflow is discharged from the crosswind device, three regions can be found: the core velocity region, the mixing region, and the low-speed region. The airflow in the core region changes smoothly without significant fluctuations; Within the range defined by diameter d=0.8D on the interested cross-section, as the wind speed increases, the maximum velocity difference gradually increases and the velocity non-uniformity gradually decreases. The research results can provide theoretical and technical bases for engine crosswind tests.
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