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某小型风扇内进口总压畸变引起流动损失分析
引用本文:孙鹏,冯国泰.某小型风扇内进口总压畸变引起流动损失分析[J].航空动力学报,2007,22(2):245-250.
作者姓名:孙鹏  冯国泰
作者单位:哈尔滨工业大学,能源科学与工程学院,哈尔滨,150001
摘    要:采用数值模拟方法对方波形式的进口总压畸变对风扇流场的影响进行了全三维非定常数值模拟.详细分析了畸变造成的动静叶栅流道内部流动损失的形式和原因.分析表明,动静叶流道内的损失在畸变和非畸变区域向下游疏运的方式不同.在动叶根部和中径区域流动损失的主要形式是疏运损失和掺混损失.畸变会使多种损失相叠加.在静叶中,畸变会在中径以下区域造成大范围的漩涡,造成回流,从而使损失增加.

关 键 词:航空、航天推进系统  数值模拟  风扇  总压畸变  流动损失  小型风扇  进口  总压畸变  流动损失  损失分析  small  distortion  pressure  total  inlet  induced  loss  flow  回流  范围  动静叶  叠加  掺混损失  变区域  中径
文章编号:1000-8055(2007)02-0245-06
收稿时间:1/4/2006 12:00:00 AM
修稿时间:2006年1月4日

Analysis of flow loss induced by inlet total pressure distortion in a small fan
SUN Peng and FENG Guo-tai.Analysis of flow loss induced by inlet total pressure distortion in a small fan[J].Journal of Aerospace Power,2007,22(2):245-250.
Authors:SUN Peng and FENG Guo-tai
Institution:School of Energy Science and Engineering, Harbin Institute of Technology, Harbin 150001, China;School of Energy Science and Engineering, Harbin Institute of Technology, Harbin 150001, China
Abstract:Numerical simulation of the unsteady flow field in a small fan using time-accurate three-dimensional Navier-Stokes solver was carried out.The numerical simulation focused on a small fan with inlet square wave total pressure distortion.The pattern and causation of flow loss caused by the pressure distortion in rotor and stator were analyzed.It is found that the influence of distortion is different at different radial positions.In the hub area,transportation-loss and mixing-loss are the main loss patterns.Distortion not only complicates them but also strengthens them.Especially in stator,inlet total pressure distortion induces large-scale vortex,which causes backflow and increases the loss.Finally,the details of flow loss both distorted and non-distorted flow fields are described and analyzed.
Keywords:aerospace propulsion system  numerical method  fan  total pressure distortion  flow loss
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