Analysis of the characteristic acoustic tones of an impinging jet
Analysis of the characteristic acoustic tones of an impinging jet
The acoustic emission of a supersonic jet is an interesting and fundamental issue due to the several technological applications and the diverse physical aspects to be still clarified. An experimental analysis of the characteristic acoustic tones of a supersonic impinging jet has been carried out with a particular attention on the effect of the nozzle pressure ratio and the distance of the impinging surface. The screech tones, typical of an imperfectly expanded supersonic free jet, have been first investigated to have an idea of the deflection from the free jet behavior due to the impinging surface. Then the analysis has been focused on smaller distances of the impinging plate from the jet exit to evaluate the behavior of the impinging tones. The difference between screech and impinging tones, due to the different interactions in the generating feedback mechanism, has been observed.
88
American Institute of Aeronautics and Astronautics
Sinibaldi, Giorgia
10078c28-4f5b-4a45-982b-9911a11ed43b
Lacagnina, Giovanni
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Marino, Luca
87dadbc6-1ae4-4732-99d8-068a0b88a8f7
Romano, Giovanni Paolo
ae4ff7ee-71ee-4ea7-8b53-b16f52547a30
2013
Sinibaldi, Giorgia
10078c28-4f5b-4a45-982b-9911a11ed43b
Lacagnina, Giovanni
b6c548d0-38b3-4f0f-9f0a-9849cb910113
Marino, Luca
87dadbc6-1ae4-4732-99d8-068a0b88a8f7
Romano, Giovanni Paolo
ae4ff7ee-71ee-4ea7-8b53-b16f52547a30
Sinibaldi, Giorgia, Lacagnina, Giovanni, Marino, Luca and Romano, Giovanni Paolo
(2013)
Analysis of the characteristic acoustic tones of an impinging jet.
In 19th AIAA/CEAS Aeroacoustics Conference.
American Institute of Aeronautics and Astronautics.
.
Record type:
Conference or Workshop Item
(Paper)
Abstract
The acoustic emission of a supersonic jet is an interesting and fundamental issue due to the several technological applications and the diverse physical aspects to be still clarified. An experimental analysis of the characteristic acoustic tones of a supersonic impinging jet has been carried out with a particular attention on the effect of the nozzle pressure ratio and the distance of the impinging surface. The screech tones, typical of an imperfectly expanded supersonic free jet, have been first investigated to have an idea of the deflection from the free jet behavior due to the impinging surface. Then the analysis has been focused on smaller distances of the impinging plate from the jet exit to evaluate the behavior of the impinging tones. The difference between screech and impinging tones, due to the different interactions in the generating feedback mechanism, has been observed.
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Published date: 2013
Venue - Dates:
19th AIAA/CEAS Aeroacoustics Conference, , Berlin, Germany, 2013-05-27 - 2013-05-29
Identifiers
Local EPrints ID: 420590
URI: http://eprints.soton.ac.uk/id/eprint/420590
PURE UUID: f511c296-0085-46dc-9bc4-19508810b3bc
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Date deposited: 10 May 2018 16:30
Last modified: 28 Jul 2022 18:51
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Contributors
Author:
Giorgia Sinibaldi
Author:
Giovanni Lacagnina
Author:
Luca Marino
Author:
Giovanni Paolo Romano
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