Airfoil Trailing-Edge Noise Reduction by Application of Finlets
نویسندگان
چکیده
This experimental study investigates the effect of biologically inspired finlets on reduction trailing-edge noise a NACA 0012 airfoil. At chord-based Reynolds number 400,000, far...
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ژورنال
عنوان ژورنال: AIAA Journal
سال: 2021
ISSN: ['0001-1452', '1533-385X', '1081-0102']
DOI: https://doi.org/10.2514/1.j060699