Rod-Airfoil Interaction Noise Reduction Using Leading Edge Serrations-Reference-Cited by-同舟云学术

Rod-Airfoil Interaction Noise Reduction Using Leading Edge Serrations

Published:2015-06-18 Issue: Volume: Page:
ISSN:
Container-title:21st AIAA/CEAS Aeroacoustics Conference
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Author:

Chen Weijie¹,Qiao Weiyang¹,Wang Liangfeng¹,Tong Fan¹,Wang Xunnian²

Affiliation:

1. Northwestern Polytechnical University

2. State Key Laboratory of Aerodynamics

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2015-3264

Reference38 articles.

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2. Leading-edge tubercles delay stall on humpback whale (Megaptera novaeangliae) flippers

3. Experimental Evaluation of Sinusoidal Leading Edges

4. Effects of Leading-Edge Protuberances on Airfoil Performance

5. 5Stanway, M. J. "Hydrodynamic Effects of Leading-Edge Tubercles on Control Surfaces and in Flapping Foil Propulsion," Ph.D. Dissertation,Massachusetts Institute of Technology, Cambridge, MA, 2008.

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2. Permeable Leading Edges for Airfoil and Fan Noise Reduction in Disturbed Inflow;AIAA Journal;2021-12

3. Reducing Aerodynamic Noise in a Rod-Airfoil Using Suction and Blowing Control Method;International Journal of Applied Mechanics;2020-05

4. Effect of Inflow Conditions on the Noise Reduction Through Leading Edge Serrations;AIAA Journal;2019-09

5. Statistical–Empirical Modeling of Airfoil Noise Subjected to Leading-Edge Serrations;AIAA Journal;2017-09