Influence of cross-section on the aeolian tone: a numerical study in the laminar regime-Reference-Cited by-同舟云学术

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Influence of cross-section on the aeolian tone: a numerical study in the laminar regime

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

Author:

Pinto Wagner J.¹,Margnat Florent¹,Gervais Yves¹

Affiliation:

1. Institut Pprime

Publisher

American Institute of Aeronautics and Astronautics

Reference68 articles.

1. x=d -1 0 1 2 3 -1 -0.5

2. 0 # " x=d -1 0 1 2 3 -1 -0.5

3. A 9.3718 2.9877 2.6879 4.24700 B 2.2678 1.1798 0.9925 1.35423

4. elip 0.55 0.541 5.1644 1.1420 4.5207 1.2447 2.5548 losn 0.90 0.636 3.1171 0.6979 3.6152 1.6027 1.8299 rect 0.40 0.596 8.7540 1.5702 5.8863 1.1957 3.0869 trib 1.20 0.995 3.3002 0.5234 3.4555 1.4073 1.2965 trif 1.20 0.427 1.4155 0.5234 0.6986 0.6689 0.5331

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Cylinder aeroacoustics: experimental study of the influence of cross-section shape on spanwise coherence length;Acta Acustica;2023

2. Influence of cylinder breadth and shape on the onset of flow unsteadiness and the aeolian tone level;Computers & Fluids;2021-10

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