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...
| Main Authors: | , , , |
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| פורמט: | Article |
| שפה: | zho |
| יצא לאור: |
Editorial Department of Advances in Aeronautical Science and Engineering
2019-06-01
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| סדרה: | Hangkong gongcheng jinzhan |
| נושאים: | |
| גישה מקוונת: | http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2018103?st=article_issue |