Experimental investigation of wing with vortex generators

Authors

  • Є.П. Ударцев National Aviation University
  • О.Г. Щербонос National Aviation University

DOI:

https://doi.org/10.18372/2306-1472.42.1810

Keywords:

big angels of attack, vortex generators, wind tunnel

Abstract

 The idea of research of the organized vortex flow of a wing for the purpose of perfection of aerodynamic characteristics on the big angels of attack develops. The wing with vortex generators in the form of flows on a forward edge in low velocity wind tunnel was with that end in view investigated. It is shown, that the organized vortex flow of a wing with vortex generators on a forward edge practically does not change aerodynamic characteristics at small angels of attack and strongly influences on the big angels of attack, increasing the maximum elevating force and improving momentum characteristics at small change of drag.

Author Biographies

Є.П. Ударцев, National Aviation University

д.т.н., проф.

О.Г. Щербонос, National Aviation University

м.н.с.

References

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How to Cite

Ударцев, Є., & Щербонос, О. (2010). Experimental investigation of wing with vortex generators. Proceedings of National Aviation University, 42(1), 45–47. https://doi.org/10.18372/2306-1472.42.1810

Issue

Section

MODERN AVIATION AND SPACE TEHNOLOGY