Boundary Layer Numerical Research of a Laminar Flow Induced by a Row of Perforations Suction

Governed by: Ministry of Industry and Information Technology of the People's Republic of China
Sponsored by: Northwestern Polytechnical University Chinese Society Aeronautics and Astronautics
Address: Aviation Building,Youyi Campus, Northwestern Polytechnical University

Home > Archive>Volume 2, Issue 1, 2011 >12-18

PDF HTML XML Export Cite reminder

Boundary Layer Numerical Research of a Laminar Flow Induced by a Row of Perforations Suction
DOI:
                        
Author:
                        
Affiliation:Yan Zhijiang,Liu Peiqing,Duan Huishen,Liu Jie(School of Aeronautic Science and Engineering,Beijing University of Aeronautics and Astronautics,Beijing 100191,China)
Clc Number:V211.3
Fund Project:

Article

Figures

Metrics

Reference

Cited by

Materials

Comments

Abstract:

Combining the characteristics of three-dimensional laminar flow induced by single perforation suction,in this paper,boundary layer of a three-dimensional laminar flow induced by a row of perforations suction is simulated by using Fluent as numerical solver.The effect of different perforation spacing and suction parameters on flow field structure is then studied.The final results show that a vertical vortex pair will interact and come into being periodic shedding horseshoe-shape vortex when the perforation s...

Reference

Cited by

Get Citation

Yan Zhijiang, Liu Peiqing, Duan Huishen, Liu Jie. Boundary Layer Numerical Research of a Laminar Flow Induced by a Row of Perforations Suction[J]. Advances in Aeronautical Science and Engineering,2011,2(1):12-18

Copy

Article Metrics

Abstract:
PDF:
HTML:
Cited by:

History

Received:
Revised:
Adopted:
Online: January 13,2012
Published:

Get Citation

Share

Article Metrics

History