The Influence of Reynolds Number on Boundary Layer Development and Stall Characteristics of Airfoil

Airfoil stall and its boundary layer development are fundamental scientific issues in aircraft design. For the trailing edge stall airfoil, The transition model coupled the Mentor <i>k</i> -<i>ω</i> SST model with the disturbance amplification factor transport equation is use...

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Bibliographic Details
Published in:	Hangkong gongcheng jinzhan
Main Authors:	Zhang Yanjun, Zhao Ke, Zhang Tongxin, Chen Lili
Format:	Article
Language:	Chinese
Published:	Editorial Department of Advances in Aeronautical Science and Engineering 2019-06-01
Subjects:	reynolds number airfoil stall boundary layer transition separation bubble turbulence model
Online Access:	http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2018103?st=article_issue

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