Control of self-induced roll oscillations using the sinusoidal leading-edge for low-aspect-ratio wings
A study on attenuating the self-induced roll oscillations of low-aspect-ratio flat-plate wings was conducted experimentally in a wind tunnel facility using a bionic flow control approach of the sinusoidal leading-edge (SLE). It was found that the effectiveness of the SLE on roll attenuation strongly...
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Published in | Experiments in fluids Vol. 61; no. 7 |
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Main Authors | , , , , , , , |
Format | Journal Article |
Language | English |
Published |
Berlin/Heidelberg
Springer Berlin Heidelberg
2020
Springer Nature B.V |
Subjects | |
Online Access | Get full text |
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