Analysis of extremal lift behavior of a semicircular airfoil in a turbulent airflow at a near-zero angle of attack

S. A. Isaev, J. J. Miau, A. G. Sudakov, A. E. Usachov

研究成果: Article同行評審

12 引文 斯高帕斯(Scopus)

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
頁(從 - 到)737-739
頁數3
期刊Technical Physics Letters
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)

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