摘要
The experimentally discovered phenomenon of lift drop for a semicircular airfoil in a turbulent airflow at a near-zero angle of attack has been numerically analyzed with multiblock computational technologies using a shear-stress-transfer model modified with allowance for the curvature of flow lines.
原文 | English |
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頁(從 - 到) | 737-739 |
頁數 | 3 |
期刊 | Technical Physics Letters |
卷 | 41 |
發行號 | 8 |
DOIs | |
出版狀態 | Published - 2015 8月 4 |
All Science Journal Classification (ASJC) codes
- 物理與天文學(雜項)