Journal article
Angle of attack effects on the induced structural loads of a weapons bay
- Abstract:
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Aero-acoustic analysis was conducted on a weapons bay numerical model with doors, incorporating radar cross section reduction features. The effect of the angle of attack on the aero-acoustic response of the cavity was analysed at Mach numbers of 0.85 and 1.20. It was found that incidence influenced both mean-flow features and acoustic response. Further, linear and angular accelerations induced by the flow on the bay doors revealed potential adverse fluid–structure coupling when the results were compared with modal analysis. Again, the angle of attack did influence the aeroacoustic effects on the cavity door structure.
- Publication status:
- Published
- Peer review status:
- Peer reviewed
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- Files:
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(Preview, Version of record, pdf, 6.9MB, Terms of use)
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- Publisher copy:
- 10.1007/s42496-024-00240-6
Authors
- Publisher:
- Springer
- Journal:
- Aerotecnica Missili and Spazio More from this journal
- Volume:
- 104
- Issue:
- 5
- Pages:
- 387-414
- Publication date:
- 2024-12-03
- Acceptance date:
- 2024-11-11
- DOI:
- EISSN:
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2524-6968
- ISSN:
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0365-7442
- Language:
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English
- Keywords:
- Pubs id:
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2072643
- Local pid:
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pubs:2072643
- Deposit date:
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2025-02-04
Terms of use
- Copyright holder:
- Bacci et al.
- Copyright date:
- 2024
- Rights statement:
- Copyright © 2024, The Author(s). This article is licensed under a Creative Commons Attribution 4.0 International License, which permits use, sharing, adaptation, distribution and reproduction in any medium or format, as long as you give appropriate credit to the original author(s) and the source, provide a link to the Creative Commons licence, and indicate if changes were made. The images or other third party material in this article are included in the article's Creative Commons licence, unless indicated otherwise in a credit line to the material. If material is not included in the article's Creative Commons licence and your intended use is not permitted by statutory regulation or exceeds the permitted use, you will need to obtain permission directly from the copyright holder. To view a copy of this licence, visit http://creativecommons.org/licenses/by/4.0/.
- Licence:
- CC Attribution (CC BY)
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