Airfoil self-noise reduction using fractal-serrated trailing edge
Airfoil self-noise reduction using fractal-serrated trailing edge
American Institute of Aeronautics and Astronautics
Hasheminejad, Seyed Mohammad
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Chong, Tze Pei
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Joseph, Phillip
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Lacagnina, Giovanni
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25 June 2018
Hasheminejad, Seyed Mohammad
df18e919-7ad3-431b-8d25-82949e839ac5
Chong, Tze Pei
5f980a6b-5e53-4491-9920-c663092ad9e7
Joseph, Phillip
9c30491e-8464-4c9a-8723-2abc62bdf75d
Lacagnina, Giovanni
b6c548d0-38b3-4f0f-9f0a-9849cb910113
Hasheminejad, Seyed Mohammad, Chong, Tze Pei, Joseph, Phillip and Lacagnina, Giovanni
(2018)
Airfoil self-noise reduction using fractal-serrated trailing edge.
In 24th AIAA/CEAS Aeroacoustics Conference.
American Institute of Aeronautics and Astronautics..
(doi:10.2514/6.2018-3132).
Record type:
Conference or Workshop Item
(Paper)
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e-pub ahead of print date: 24 June 2018
Published date: 25 June 2018
Venue - Dates:
24th AIAA/CEAS Aeroacoustics Conference, , Atlanta, United States, 2018-06-25 - 2018-06-29
Identifiers
Local EPrints ID: 422193
URI: http://eprints.soton.ac.uk/id/eprint/422193
PURE UUID: 9e100f84-7ac7-4fc9-9fec-d394385853f1
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Date deposited: 18 Jul 2018 16:31
Last modified: 15 Mar 2024 20:40
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Contributors
Author:
Seyed Mohammad Hasheminejad
Author:
Tze Pei Chong
Author:
Giovanni Lacagnina
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