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

Research output: Contribution to journalArticlepeer-review

10 Citations (Scopus)

Abstract

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.

Original languageEnglish
Pages (from-to)737-739
Number of pages3
JournalTechnical Physics Letters
Volume41
Issue number8
DOIs
Publication statusPublished - 2015 Aug 4

All Science Journal Classification (ASJC) codes

  • Physics and Astronomy (miscellaneous)

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