Zobrazeno 1 - 8 of 8 pro vyhledávání: '"Matthew Szoke"'
1
Design and performance of an aeroacoustic wind tunnel facility at the University of Bristol
Autor: Matthew Szoke, Syamir Alihan Showkat Ali, Yannick D Mayer, Mahdi Azarpeyvand, Hasan Kamliya Jawahar
Publikováno v: Mayer, Y D, Kamliya Jawahar, H, Szoke, M, Showkat Ali, S A & Azarpeyvand, M 2019, ' Design and performance of an aeroacoustic wind tunnel facility at the University of Bristol ', Applied Acoustics, vol. 155, pp. 358-370 . https://doi.org/10.1016/j.apacoust.2019.06.005
This paper provides an overview of the design and performance of the new aeroacoustic wind tunnel facility at the University of Bristol. The purpose of the facility is to enable near- and far-field acoustic and aerodynamic studies on a variety of dif
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::8725a9a868f252c356236e81ec010937
https://research-information.bris.ac.uk/ws/files/202535613/Design_and_Performance_of_an_Aeroacoustic_Wind_Tunnel_Facilty_at_the_University_of_Bristol.pdf
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2
Trailing-edge flow manipulation using streamwise finlets
Autor: Ali A. Dehghan, Reza Maryami, Matthew Szoke, Abbas Afshari, Mahdi Azarpeyvand
Publikováno v: Afshari, A, Azarpeyvand, M, Dehghan, A A, Szoke, M & Maryami, R 2019, ' Trailing-edge flow manipulation using streamwise finlets ', Journal of Fluid Mechanics, vol. 870, pp. 617-650 . https://doi.org/10.1017/jfm.2019.249
The use of streamwise finlets as a passive flow and aerodynamic noise-control technique is considered in this paper. A comprehensive experimental investigation is undertaken using a long flat plate, and results are presented for the boundary layer an
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::c480b75fc609274469586faf3884ea12
https://research-information.bris.ac.uk/en/publications/e113412e-9e10-4cdb-a29c-385bc1441bc3
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3
Uniform Suction for the Reduction of the Trailing-Edge Noise
Autor: Matthew Szoke, Daniele Fiscaletti, Mahdi Azarpeyvand
Publikováno v: Szoke, M, Azarpeyvand, M & Fiscaletti, D 2019, Uniform Suction for the Reduction of the Trailing Edge Noise . in Proceedings of the 25th AIAA/CEAS Aeroacoustics Conference : 20-23 May 2019 Delft, The Netherlands . American Institute of Aeronautics and Astronautics Inc. (AIAA) . https://doi.org/10.2514/6.2019-2651
Uniform inclined suction from a spanwise slot is applied upstream of a trailing edge on a zero pressure gradient at plate with the aim of reducing trailing edge noise. The effects of the flow treatment on the turbulence statistics are experimentally
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::d80314c323a5c50ad245c5c0118d2b66
https://doi.org/10.2514/6.2019-2651
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4
The Use of Micro-jets for Airfoil Self-noise Control
Autor: Daniele Fiscaletti, Matthew Szoke, Mahdi Azarpeyvand
Publikováno v: Szoke, M, Fiscaletti, D & Azarpeyvand, M 2018, The Use of Micro-jets for Airfoil Self-noise Control . in 24th AIAA/CEAS Aeroacoustics Conference 2018 : Proceedings of a meeting held 25-29 June 2018, Atlanta, Georgia, USA. Held at the AIAA Aviation Forum 2018 . vol. 3, American Institute of Aeronautics and Astronautics Inc. (AIAA) . https://doi.org/10.2514/6.2018-3141
The current work is an experimental investigation on the use of open-loop flow control techniques to reduce trailing edge noise of a flat plate. An array of inclined transverse jet nozzles is placed upstream of the trailing edge, with the aim of cont
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::235e7272efe063633527b4679f57a19f
https://research-information.bris.ac.uk/en/publications/15ace039-03c8-4175-8def-d2c3b72c8236
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7
Active Flow Control Methods for the Reduction of Trailing Edge Noise
Autor: Matthew Szoke, Mahdi Azarpeyvand
Publikováno v: Szoke, M & Azarpeyvand, M 2017, Active Flow Control Methods for the Reduction of Trailing Edge Noise . in 23rd AIAA/CEAS Aeroacoustics Conference ., AIAA 2017-3004, American Institute of Aeronautics and Astronautics Inc. (AIAA), 23rd AIAA/CEAS Aeroacoustics Conference, Denver, CO, United States, 5/06/17 . https://doi.org/10.2514/6.2017-3004
The possibility of trailing edge noise reduction using active flow control is addressed in this paper. The boundary layer is altered with the help of uniform perpendicular and inclined flow injection and suction on a long flat plate upstream of a sha
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::c69c93ed56e0ca0342ab4c4e4ae1e894
https://hdl.handle.net/1983/5a83b273-1bad-451c-aedb-61589e835c1e
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8
Effects of Streamwise Surface Treatments on Trailing Edge Noise Reduction
Autor: Abbas Afshari, Mahdi Azarpeyvand, Matthew Szoke, Ali A. Dehghan
Publikováno v: Afshari, A, Azarpeyvand, M, Dehghan, A A & Szoke, M 2017, Effects of Streamwise Surface Treatments on Trailing Edge Noise Reduction . in 23rd AIAA/CEAS Aeroacoustics Conference ., AIAA 2017-3499, American Institute of Aeronautics and Astronautics Inc. (AIAA) . https://doi.org/10.2514/6.2017-3499
The use of surface treatments as a passive flow control method for trailing edge noise reduction is considered in this paper. In order to investigate the effects of different types of surface treatments on surface pressure fluctuations, eddy convecti
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::76d00161cb6fb5ae439629b6cba388fe
https://doi.org/10.2514/6.2017-3499
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