| Citation: | ZHANG Peng, CHENG Rixin, LI Yonghong, et al. Numerical study on the control of airfoil stall with bio-inspired herringbone groove array[J]. Journal of Aerospace Power, 2024, 39（11）：20230415 doi: 10.13224/j.cnki.jasp.20230415
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Taking the NACA0012 airfoil as the research object, the control rules and physical mechanisms of bio-inspired herringbone groove array on airfoil stall were explored through numerical simulations. The herringbone groove array was placed on the airfoil's upper surface near the trailing edge, and the effects of groove depth and deflection angle on the control effectiveness were investigated. The results showed that different designs of herringbone groove array can effectively broaden the stable operating range of the airfoil, and the implementation of herringbone groove array with a depth of only
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