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JCR 2016
جستجوی مقالات
پنجشنبه 20 آذر 1404
Journal of Applied Fluid Mechanics
، جلد ۱۷، شماره ۱۲، صفحات ۲۷۰۸-۲۷۱۹
عنوان فارسی
چکیده فارسی مقاله
کلیدواژههای فارسی مقاله
عنوان انگلیسی
Experimental Investigation of Aerodynamic Noise Characteristics of Tandem Asymmetric Airfoils Across Varied Angles of Attack
چکیده انگلیسی مقاله
This paper experimentally investigates the aerodynamic noise characteristics of a tandem asymmetric airfoil-airfoil at different angles of attack in the 0.5 m×0.4 m acoustic wind tunnel at Wenzhou University. Based on the airfoil chord length and the wind speed, the Reynolds number ranges between 2.2×10
5
and 3.5×10
5
. Meanwhile, the attack angle (α
1
and α
2
) of both tandem airfoils varies between 0~20°, and the noise is measured using a far/near-field microphone array. The experimental results indicate that when the attack angle α
1
of the upstream airfoil is small (α
1
<15°), its wake hardly interacts with the downstream airfoil, and the noise source is mainly concentrated at the trailing edge of the upstream airfoil. When the attack angle α
1
is larger than 15°, the upstream wake interacts with the downstream airfoil, the noise radiates from the leading edge of the downstream airfoil, and the source location varies slightly at different frequencies. Compared to the upstream attack angle α
1
, the downstream airfoil attack angle α
2
has less impact on the aerodynamic noise of the tandem airfoils. Additionally, the particle imaging velocimetry technique is employed to measure the flow field characteristics and analyze the mechanism of noise production.
کلیدواژههای انگلیسی مقاله
Aerodynamic noise Angles of attack Tandem asymmetric airfoil Tone noise Turbulence,surface interaction
نویسندگان مقاله
W. Shi |
College of Mechanical and Electrical Engineering, Wenzhou University, Wenzhou, Zhejiang 325035 China
J. Zhou |
College of Mechanical and Electrical Engineering, Wenzhou University, Wenzhou, Zhejiang 325035 China
J. Zhou |
College of Mechanical and Electrical Engineering, Wenzhou University, Wenzhou, Zhejiang 325035 China
Z. Chen |
Key Laboratory of Aerodynamic Noise Control, China Aerodynamics Research and Development Center, Mianyang, Sichuan, 621000, China
نشانی اینترنتی
https://www.jafmonline.net/article_2524_0b1281ce038d19df308d9a0212852236.pdf
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