Controlling aerodynamic noise of macroscopic point array structure on leading edge of airfoil
|更新时间:2026-01-28
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Controlling aerodynamic noise of macroscopic point array structure on leading edge of airfoil
“In the aviation field, researchers have designed the NACA0012 airfoil leading edge lattice turbulence structure and verified its noise reduction effect through acoustic wind tunnel testing, providing new ideas for airfoil noise reduction design.”
Journal of Jilin University(Engineering and Technology Edition)Vol. 56, Issue 1, Pages: 86-95(2026)
SHEN Chun,LI Zhuang,MENG Jin,et al.Controlling aerodynamic noise of macroscopic point array structure on leading edge of airfoil[J].Journal of Jilin University(Engineering and Technology Edition),2026,56(01):86-95.
SHEN Chun,LI Zhuang,MENG Jin,et al.Controlling aerodynamic noise of macroscopic point array structure on leading edge of airfoil[J].Journal of Jilin University(Engineering and Technology Edition),2026,56(01):86-95. DOI: 10.13229/j.cnki.jdxbgxb.20240669.
Controlling aerodynamic noise of macroscopic point array structure on leading edge of airfoil