A theoretical model of fuselage pressure levels due to fan tones radiated from the intake of an installed turbofan aero-engine
- Submitting institution
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University of Southampton
- Unit of assessment
- 12 - Engineering
- Output identifier
- 41349616
- Type
- D - Journal article
- DOI
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10.1121/1.5038263
- Title of journal
- Journal of the Acoustical Society of America
- Article number
- -
- First page
- 3394
- Volume
- 143
- Issue
- -
- ISSN
- 0001-4966
- Open access status
- Compliant
- Month of publication
- June
- Year of publication
- 2018
- URL
-
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- Supplementary information
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- Request cross-referral to
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- Output has been delayed by COVID-19
- No
- COVID-19 affected output statement
- -
- Forensic science
- No
- Criminology
- No
- Interdisciplinary
- No
- Number of additional authors
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2
- Research group(s)
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-
- Proposed double-weighted
- No
- Reserve for an output with double weighting
- No
- Additional information
- New theoretical method for turbofan installation acoustics - related previous work was for noise radiated by propellers. Collaborative work with funding from Rolls-Royce plc via the Rolls-Royce University Technology Centre in Gas Turbine Noise. Follow-up funding was secured in the project ARTEM “Aircraft noise Reduction Technologies and related Environment iMpact”, EU Horizon 2020 grant No. 769 350. A key aim of the follow-up work is to increase the technology readiness level of the method for transfer to Rolls-Royce plc.
- Author contribution statement
- -
- Non-English
- No
- English abstract
- -