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

S. A. Isaev, Jiun-Jih Miau, A. G. Sudakov, A. E. Usachov

Research output: Contribution to journalArticle

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

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zero angle of attack
airfoils
allowances
shear stress
curvature

All Science Journal Classification (ASJC) codes

  • Physics and Astronomy (miscellaneous)

Cite this

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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.",
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Analysis of extremal lift behavior of a semicircular airfoil in a turbulent airflow at a near-zero angle of attack. / Isaev, S. A.; Miau, Jiun-Jih; Sudakov, A. G.; Usachov, A. E.

In: Technical Physics Letters, Vol. 41, No. 8, 04.08.2015, p. 737-739.

Research output: Contribution to journalArticle

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AU - Miau, Jiun-Jih

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AU - Usachov, A. E.

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