Wake Modification and Noise Emission of Serrated NACA 65(12)-10 at Moderate Reynolds Number-Reference-Cited by-同舟云学术

Wake Modification and Noise Emission of Serrated NACA 65(12)-10 at Moderate Reynolds Number

Published:2021-09 Issue:5 Volume:34 Page:04021056
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Chen Nanshu¹^ORCID,Liu Hanru²^ORCID,Liu Qian³,Wang Yangang⁴

Affiliation:

1. Ph.D. Student, School of Power and Energy, Northwestern Polytechnical Univ., Xi’an, Shaanxi 710129, PR China; Research & Development Institute of Northwestern Polytechnical Univ. in Shenzhen, Shenzhen, Guangdong 518057, PR China. ORCID: .

2. Associate Professor, School of Power and Energy, Northwestern Polytechnical Univ., Xi’an, Shaanxi 710129, PR China; Research & Development Institute of Northwestern Polytechnical Univ. in Shenzhen, Shenzhen, Guangdong 518057, PR China (corresponding author). ORCID: .

3. Master’s Student, School of Power and Energy, Northwestern Polytechnical Univ., Xi’an, Shaanxi 710129, PR China.

4. Professor, School of Power and Energy, Northwestern Polytechnical Univ., Xi’an, Shaanxi 710129, PR China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001299

Reference35 articles.

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3. Arina R. R. D. R. Rinaldi A. Iob and D. Torzo. 2012. “Numerical study of self-noise produced by an airfoil with trailing edge serrations.” In Proc. 18th AIAA/CEAS Aeroacoustics Conf. (33rd AIAA Aeroacoustics Conf.) AIAA 2012-2184. Reston VA: American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-2184.

4. Benefits of curved serrations on broadband trailing-edge noise reduction

5. Noise reduction mechanisms of sawtooth and combed-sawtooth trailing-edge serrations

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