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- W4384695250 abstract "Studying the sonic boom phenomenon is an ongoing interest for researchers and engineers to ensure the possibility of supersonic flights for civil aircraft, allowing faster air travel for everyone. Research in sonic boom reduction was previously done by general aircraft shape optimization and engine design. This research focuses on wing geometry modification and its effects on sonic boom loudness reduction. A supersonic aircraft based on the supersonic airliner concept (SSA) was created to learn how the sonic boom loudness and overpressures change by applying wing geometry sensitivity analyses. The sensitivity analyses include wing geometry changes, wing sweep angle changes, and wing translation while maintaining the same aircraft lift. The volume of the selected aircraft is then matched to the base SSA model for geometric parity. A 2.88 PLdB reduction in sonic boom loudness was achieved while maintaining the same volume and lift as the base SSA model." @default.
- W4384695250 created "2023-07-20" @default.
- W4384695250 creator A5056455843 @default.
- W4384695250 date "2023-07-18" @default.
- W4384695250 modified "2023-10-16" @default.
- W4384695250 title "Reduction of Sonic Boom Loudness Level in Supersonic Aircraft by Optimization of Wing Geometry and Positioning" @default.
- W4384695250 doi "https://doi.org/10.22215/etd/2023-15474" @default.
- W4384695250 hasPublicationYear "2023" @default.
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