Výsledky vyhledávání - "Philip C. Woodhead"

Frequency-Targetable Aerofoil Self-Noise Reduction

Autor: Jan G. Wissink, Tze Pei Chong, Phillip Joseph, Philip C. Woodhead, Paruchuri Chaitanya

Publikováno v: AIAA AVIATION 2021 FORUM.

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::568102aa69aab241b415ff1a06327f1c
https://doi.org/10.2514/6.2021-2229

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Aerofoil Self Noise Radiations Subjected to Serration Flap Angles

Autor: Tze Pei Chong, Phillip Joseph, Alexandros Vathylakis, Philip C. Woodhead

Copyright © 2021 The Author(s). Besides the investigation of the aeroacoustics responses of an asymmetric aerofoil subjected to serrated trailing edge flap angles from negative (flap-down) to positive (flap-up), this paper also provides a new perspe

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::a83d15586c91000d871a4efbf04456a1
https://bura.brunel.ac.uk/handle/2438/22829

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On the Double-Rooted Trailing Edge Serration

Autor: Tze Pei Chong, Jan G. Wissink, Philip C. Woodhead, Phillip Joseph

Publikováno v: 25th AIAA/CEAS Aeroacoustics Conference

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::7b17fe6586efb8730ae07e7d66fc8f59
https://doi.org/10.2514/6.2019-2436

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Exploiting the Misalignment of the Serrated Trailing Edge for Improved Aerofoil Broadband Noise Reduction

Autor: Jan G. Wissink, Tze Pei Chong, Philip C. Woodhead

Publikováno v: AIAA Aviation
Scopus-Elsevier

This paper presents the experimental results of adding variable flap angles to the serrated trailing edges and their effects on the self-noise radiation of an aerofoil. The investigation included aeroacoustics and wake flow measurements on an NACA 65

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::2338d5116437474db24f6a05fb59b7ad
https://doi.org/10.2514/6.2017-4175

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Leading edge noise reduction of thin aerofoil by the straight and curved serrations of the add-on type

Autor: Philip C. Woodhead, Auris Juknevicius, Tze Pei Chong

Publikováno v: AIAA Aviation
Scopus-Elsevier

This paper presents the experimental results of the effect of add-on type leading edge serrations on the aeroacoustic performance of a symmetrical NACA0008 aerofoil. The focus is on the turbulence-leading edge interaction broadband noise. Tests have

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::67de5ed97a9dd5e3bdf0af438f215176
http://bura.brunel.ac.uk/handle/2438/16820

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