Exploring angle-of-attack effects in the aero-acoustic response of a weapons bay at transonic and supersonic Mach number
dc.contributor.author | Bacci, David | |
dc.contributor.author | Saddington, Alistair J. | |
dc.date.accessioned | 2022-07-13T14:07:43Z | |
dc.date.available | 2022-07-13T14:07:43Z | |
dc.date.issued | 2022-06-13 | |
dc.description.abstract | Numerical aero-acoustic analysis was conducted on a weapon bay model with doors, incorporating radar cross section reduction features. The effect of angle of attack on the aero-acoustic response of the cavity was analysed at a transonic Mach number of 0.85, and at a supersonic Mach number of 1.20. It was found that incidence had influence on both mean-flow features and acoustic response. Further, linear and angular accelerations induced by the flow on doors revealed potential adverse fluid-structure coupling when results were compared with modal analysis. Again, angle of attack did influence the aeroacoustic effects on the cavity door structure. | en_UK |
dc.identifier.citation | Bacci D, Saddington AJ. (2022) Exploring angle-of-attack effects in the aero-acoustic response of a weapons bay at transonic and supersonic Mach number. In: 28th AIAA/CEAS Aeroacoustics 2022 Conference, 14-17 June 2022, Southampton, UK. AIAA 2022-3008 | en_UK |
dc.identifier.eisbn | 9781624106644 | |
dc.identifier.uri | https://doi.org/10.2514/6.2022-3008 | |
dc.identifier.uri | https://dspace.lib.cranfield.ac.uk/handle/1826/18160 | |
dc.language.iso | en | en_UK |
dc.publisher | AIAA | en_UK |
dc.rights | Attribution-NonCommercial 4.0 International | * |
dc.rights.uri | http://creativecommons.org/licenses/by-nc/4.0/ | * |
dc.subject | Critical Angle of Attack | en_UK |
dc.subject | Freestream Mach Number | en_UK |
dc.subject | Modal Analysis | en_UK |
dc.subject | RADAR | en_UK |
dc.subject | Overall Sound Pressure Level | en_UK |
dc.subject | Supersonic Speed | en_UK |
dc.subject | Strouhal Numbers | en_UK |
dc.subject | Pressure Coefficient | en_UK |
dc.subject | Shear Layers | en_UK |
dc.subject | Fluid Structure Interaction | en_UK |
dc.title | Exploring angle-of-attack effects in the aero-acoustic response of a weapons bay at transonic and supersonic Mach number | en_UK |
dc.type | Conference paper | en_UK |
Files
Original bundle
1 - 1 of 1
Loading...
- Name:
- Exploring_angle-of-attack_effects-2022.pdf
- Size:
- 2.58 MB
- Format:
- Adobe Portable Document Format
- Description:
License bundle
1 - 1 of 1
No Thumbnail Available
- Name:
- license.txt
- Size:
- 1.63 KB
- Format:
- Item-specific license agreed upon to submission
- Description: