An experimental investigation of the effect of owl-inspired velvety coating on trailing edge noise-Reference-Cited by-同舟云学术

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An experimental investigation of the effect of owl-inspired velvety coating on trailing edge noise

Published:2019-05-18 Issue: Volume: Page:
ISSN:
Container-title:25th AIAA/CEAS Aeroacoustics Conference
language:
Short-container-title:

Author:

Zhou Peng¹,Lui Go Nam¹,Zhang Xin¹

Affiliation:

1. Hong Kong University of Science and Technology

Publisher

American Institute of Aeronautics and Astronautics

Reference34 articles.

1. Lockard,D.P.,andLilley,G.M.“Theairframenoisereductionchallenge,”Tech.rep.,NASA-TM-2004-213013,2004.

2. Aerodynamic sound generation by turbulent flow in the vicinity of a scattering half plane

3. Noise due to turbulent flow past a trailing edge

4. The Silent Flight of Owls

5. Fowler,M.,andCubas,Z.S.,Biology,medicine,andsurgeryofSouthAmericanwildanimals,JohnWiley&Sons,2008.

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1. Trailing-edge fringes enable robust aerodynamic force production and noise suppression in an owl wing model;Bioinspiration & Biomimetics;2023-11-17

2. Functionalized and Biomimicked Carbon-Based Materials and Their Impact for Improving Surface Coatings for Protection and Functionality: Insights and Technological Trends;Coatings;2022-11-04

3. Effects of owl-inspired leading-edge serrations on tandem wing aeroacoustics;AIP Advances;2022-11-01

4. Design and characterization of a multifunctional low-speed anechoic wind tunnel at HKUST;Aerospace Science and Technology;2021-08

5. On the effect of velvet structures on trailing edge noise: experimental investigation and theoretical analysis;Journal of Fluid Mechanics;2021-05-25

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