Fuselage boundary-layer refraction of fan tones radiated from an installed turbofan aero-engine
Fuselage boundary-layer refraction of fan tones radiated from an installed turbofan aero-engine
Each sheet of the spreadsheet corresponds to a figure in the paper.
On each sheet is a table. In the table is numerical values used in the relevant figure.
The units are in the top left of the table.
The parameters are can be obtained from the paper.
For the cylinder plots the azimuthal displacements is along the rows and the axial displacement is columns.
University of Southampton
Gaffney, James
7d1a9e19-a1cc-4066-8d98-e9e29c2a0177
Mcalpine, Alan
aaf9e771-153d-4100-9e84-de4b14466ed7
Kingan, Michael
2d2daafa-d6d7-41aa-a9fc-2307259ac9f0
Gaffney, James
7d1a9e19-a1cc-4066-8d98-e9e29c2a0177
Mcalpine, Alan
aaf9e771-153d-4100-9e84-de4b14466ed7
Kingan, Michael
2d2daafa-d6d7-41aa-a9fc-2307259ac9f0
Gaffney, James, Mcalpine, Alan and Kingan, Michael
(2017)
Fuselage boundary-layer refraction of fan tones radiated from an installed turbofan aero-engine.
University of Southampton
doi:10.5258/SOTON/400423
[Dataset]
Abstract
Each sheet of the spreadsheet corresponds to a figure in the paper.
On each sheet is a table. In the table is numerical values used in the relevant figure.
The units are in the top left of the table.
The parameters are can be obtained from the paper.
For the cylinder plots the azimuthal displacements is along the rows and the axial displacement is columns.
Spreadsheet
JASA_JG_AMCA_MK.xlsx
- Dataset
More information
Published date: 2017
Organisations:
Education Hub, Acoustics Group, Inst. Sound & Vibration Research
Identifiers
Local EPrints ID: 400423
URI: http://eprints.soton.ac.uk/id/eprint/400423
PURE UUID: 0cb2160b-8e78-4ea8-99af-d2c3661f6e68
Catalogue record
Date deposited: 10 Feb 2017 12:45
Last modified: 05 Nov 2023 02:36
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Contributors
Creator:
James Gaffney
Creator:
Michael Kingan
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