Aerospace, Volume 5, Issue 4
2018 December - 31 articles
Cover Story: A combined numerical and experimental approach was employed to investigate active flow control and its interplay with separation and transition in laminar separation bubbles. Experiments were carried out in a wind tunnel and in free flight using an instrumented 1:5 scale model of the Aeromot 200S, which has a modified NACA 643-618 airfoil. The same airfoil was also employed in simulations and wind tunnel experiments. With the properly chosen actuation amplitudes and frequencies, the Kelvin–Helmholtz instability resulted in a strong disturbance amplification and a “roll-up” of the separated shear layer. As a result, efficient and effective laminar separation control was realized. View this paper. - Issues are regarded as officially published after their release is announced to the table of contents alert mailing list .
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