Influence of non-dimensional parameters on the tip leakage noise
Influence of non-dimensional parameters on the tip leakage noise
This paper experimentally characterises the flow behaviour within the tip gap area of a single-fixed aerofoil by studying the influence of two non-dimensional parameters. The tip leakage flow behaviour has been previously linked to the geometric ratio between the local aerofoil thickness and the tip gap size. To explore this dependency, several aerofoils characterised by different thicknesses were investigated. However, the thickness-to-gap ratio alone is not sufficient to define the tip flow behaviour, which instead can be defined by the pressure distribution along the tip of the aerofoil. The influence of the boundary layer thickness on the tip leakage flow was investigated, but it was found to have little impact. This study also provides insight into the dominant tip noise source, which is related to a shear layer instability that occurs downstream of the midchord.
Aerospace Research Central
Saraceno, Ivan
9c74b5c9-b834-43cc-b26d-9408b0534304
Cabre, Sergi Palleja
b841a96c-05d1-4f08-a197-8693cb3a3f90
Paruchuri, Chaitanya
5c1def64-6347-4be3-ac2d-b9f6a314b81d
Ganapathisubramani, Bharath
83fd359c-27c2-452d-b00a-d4b17ed419d5
8 June 2023
Saraceno, Ivan
9c74b5c9-b834-43cc-b26d-9408b0534304
Cabre, Sergi Palleja
b841a96c-05d1-4f08-a197-8693cb3a3f90
Paruchuri, Chaitanya
5c1def64-6347-4be3-ac2d-b9f6a314b81d
Ganapathisubramani, Bharath
83fd359c-27c2-452d-b00a-d4b17ed419d5
Saraceno, Ivan, Cabre, Sergi Palleja, Paruchuri, Chaitanya and Ganapathisubramani, Bharath
(2023)
Influence of non-dimensional parameters on the tip leakage noise.
In Proceedings of the AIAA AVIATION 2023 Forum.
Aerospace Research Central..
(doi:10.2514/6.2023-3838).
Record type:
Conference or Workshop Item
(Paper)
Abstract
This paper experimentally characterises the flow behaviour within the tip gap area of a single-fixed aerofoil by studying the influence of two non-dimensional parameters. The tip leakage flow behaviour has been previously linked to the geometric ratio between the local aerofoil thickness and the tip gap size. To explore this dependency, several aerofoils characterised by different thicknesses were investigated. However, the thickness-to-gap ratio alone is not sufficient to define the tip flow behaviour, which instead can be defined by the pressure distribution along the tip of the aerofoil. The influence of the boundary layer thickness on the tip leakage flow was investigated, but it was found to have little impact. This study also provides insight into the dominant tip noise source, which is related to a shear layer instability that occurs downstream of the midchord.
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Published date: 8 June 2023
Venue - Dates:
AIAA AVIATION 2023 Forum, , San Diego, United States, 2023-06-12 - 2023-06-16
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Local EPrints ID: 478740
URI: http://eprints.soton.ac.uk/id/eprint/478740
PURE UUID: 63d94398-c341-4a5f-9931-50b74970ae21
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Date deposited: 07 Jul 2023 16:52
Last modified: 17 Mar 2024 03:48
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Author:
Ivan Saraceno
Author:
Bharath Ganapathisubramani
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