Angle of Attack Effects on the Induced Structural Loads of a Weapons Bay

Abstract 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.

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Publication Details

Journal
Aerotecnica Missili & Spazio
Published
2024-12-03
DOI
https://doi.org/10.1007/s42496-024-00240-6
Primary Topic
Aerodynamics and Acoustics in Jet Flows
Type
article
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article

Angle of Attack Effects on the Induced Structural Loads of a Weapons Bay

David Bacci, A. J. Saddington
Aerotecnica Missili & Spazio
Aerodynamics and Acoustics in Jet Flows
article

Angle of Attack Effects on the Induced Structural Loads of a Weapons Bay

David Bacci, A. J. Saddington
article en

Abstract

Abstract 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.

Aerotecnica Missili & SpazioVol. 104(5)
University of Oxford (GB), Cranfield University (GB)
Life below water
Openalex Percentile: Top 65%
Aerodynamics and Acoustics in Jet Flows
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