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Numerical investigation on drag reduction effect by mass injection from porous boundary wall
  • ISSN号:1005-1120
  • 期刊名称:Transactions of Nanjing University of Aeronautics
  • 时间:2015.4.1
  • 页码:250-254
  • 分类:O35[理学—流体力学;理学—力学]
  • 作者机构:[1]Transportation Equipment and Ocean Engineering College, Dalian Maritime University, Dalian 116026, P.R. China, [2]State Key Laboratory of Ocean Engineering, Shanghai Jiao Tong University, Shanghai 200240, P.R. Chinas, [3]State Key Laboratory of Oil and Gas Reservoir Geology and Exploration, Southwest Petroleum University, Chengdu 610500, P.R. Chinas, [4]Wood Group Mustang, Shanghai 201206, P.R. China, [5]School of Naval Architecture, Dalian University of Technology, Dalian 116024, P.R. China
  • 相关基金:supported by the National Natural Science Foundation of China (Nos.51309040,51209027, 51379025,51379033); the Open Research Fund of State Key Laboratory of Ocean Engineering (Shanghai Jiao Tong University,No.1402); the Young Teachers Academic Program of SWPU (No.201499010114); the Central Financial Support of Local Key Discipline Youth Fund Project (YC319); the Fundamental Research Fund for the Central Universities(No.DMU3132015089)
  • 相关项目:无尾翼圆碟水下运动关键技术研究
中文摘要:

Interaction between the injected flow from the porous wall and the main flow can reduce drag effectively.The phenomenon is significant to the flight vehicle design.The intensive flux of injection enhances difficulty of numerical simulation and requires higher demands on the turbulence model.A turbulent boundary layer flow with mass injection through a porous wall governed by Reynolds averaged Navier-Stokers(RANS)equations is solved by using the Wilcox′s k-ωturbulence model and the obtained resistance coefficient agrees well with the experimental data.The results with and without mass injection are compared with other conditions unchanged.Velocity profile,turbulent kinetic energy and turbulent eddy viscosity are studied in these two cases.Results confirm that the boundary layer is blowing up and the turbulence is better developed with the aid of mass injection,which may explain the drag reduction theoretically.This numerical simulation may deepen our comprehension on this complex flow.

英文摘要:

Interaction between the injected flow from the porous wall and the main flow can reduce drag effectively.The phenomenon is significant to the flight vehicle design.The intensive flux of injection enhances difficulty of numerical simulation and requires higher demands on the turbulence model.A turbulent boundary layer flow with mass injection through a porous wall governed by Reynolds averaged Navier-Stokers(RANS)equations is solved by using the Wilcox′s k-ωturbulence model and the obtained resistance coefficient agrees well with the experimental data.The results with and without mass injection are compared with other conditions unchanged.Velocity profile,turbulent kinetic energy and turbulent eddy viscosity are studied in these two cases.Results confirm that the boundary layer is blowing up and the turbulence is better developed with the aid of mass injection,which may explain the drag reduction theoretically.This numerical simulation may deepen our comprehension on this complex flow.

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期刊信息
  • 《南京航空航天大学学报:英文版》
  • 主管单位:工业和信息化部
  • 主办单位:南京航空航天大学
  • 主编:宣益民
  • 地址:南京市御道街29号1016信箱
  • 邮编:210016
  • 邮箱:Tnuaa@nuaa.edu.cn
  • 电话:025-84892071
  • 国际标准刊号:ISSN:1005-1120
  • 国内统一刊号:ISSN:32-1389/V
  • 邮发代号:
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  • 被引量:205