Flow visualization study was conducted to investigate the quasi-periodical behavior of the laminar separation bubble formed on a NACA0012 airfoil at the angles of attack α=11–12
º. The Reynolds number based on the airfoil chord was Re
=1.3×10
5. At α=11.5
º, the flow over the airfoil quasi-periodically switches between a large separated flow and an attached flow with small separation near the leading edge at a frequency of about 2Hz. This attached flow resembles the flow pattern with a short bubble formed near the leading edge such as at α=10
º. Ejection of large vortices downstream was observed during the quasi-periodical switching. The flow stays attached to the airfoil surface at α=11
º. As the angle of attack is increased, the large separated flow becomes dominant. At α=12
º, the flow is completely separated largely.
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