Noise Study Auralization of an Open-Rotor Engine
Based on the performance and acoustic data files of reduced-size open-rotor engines in low-speed wind tunnels, the static sound pressure level was derived by converting the 1-foot lossless spectral density into sound-pressure-level data, the background noise was removed, and the results were correct...
| Published in: | Aerospace |
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| Main Authors: | , , , , |
| Format: | Article |
| Language: | English |
| Published: |
MDPI AG
2024-10-01
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| Subjects: | |
| Online Access: | https://www.mdpi.com/2226-4310/11/10/857 |
| _version_ | 1849684809441345536 |
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| author | Qing Zhang Siyi Jiang Xiaojun Yang Yongjia Xu Maosheng Zhu |
| author_facet | Qing Zhang Siyi Jiang Xiaojun Yang Yongjia Xu Maosheng Zhu |
| author_sort | Qing Zhang |
| collection | DOAJ |
| container_title | Aerospace |
| description | Based on the performance and acoustic data files of reduced-size open-rotor engines in low-speed wind tunnels, the static sound pressure level was derived by converting the 1-foot lossless spectral density into sound-pressure-level data, the background noise was removed, and the results were corrected according to the environmental parameters of the low-speed wind tunnels. In accordance with the requirements of Annex 16 of the Convention on International Civil Aviation Organization and Part 36 of the Civil Aviation Regulations of China on noise measurement procedures, the takeoff trajectory was physically modeled; the static noise source was mapped onto the takeoff trajectory to simulate the propagation process of the noise during takeoff; and the 24 one-third-octave center frequencies that corresponded to the SPL data were corrected for geometrical dispersion, atmospheric absorption, and Doppler effects, so that the takeoff noise could be corrected to represent a real environment. In addition, the audible processing of noise data with a 110° source pointing angle was achieved, which can be useful for enabling practical observers to analyze the noise characteristics. |
| format | Article |
| id | doaj-art-e63fddfde60a4a6e967af20cd5e844e8 |
| institution | Directory of Open Access Journals |
| issn | 2226-4310 |
| language | English |
| publishDate | 2024-10-01 |
| publisher | MDPI AG |
| record_format | Article |
| spelling | doaj-art-e63fddfde60a4a6e967af20cd5e844e82025-08-20T02:11:01ZengMDPI AGAerospace2226-43102024-10-01111085710.3390/aerospace11100857Noise Study Auralization of an Open-Rotor EngineQing Zhang0Siyi Jiang1Xiaojun Yang2Yongjia Xu3Maosheng Zhu4College of Aeronautical Engineering, Civil Aviation University of China, Tianjin 300300, ChinaSchool of Energy and Power Engineering, Beihang University, Beijing 100191, ChinaResearch Institute of Science and Technology Innovation, Civil Aviation University of China, Tianjin 300300, ChinaSchool of Energy and Power Engineering, Beihang University, Beijing 100191, ChinaCollege of Aeronautical Engineering, Civil Aviation University of China, Tianjin 300300, ChinaBased on the performance and acoustic data files of reduced-size open-rotor engines in low-speed wind tunnels, the static sound pressure level was derived by converting the 1-foot lossless spectral density into sound-pressure-level data, the background noise was removed, and the results were corrected according to the environmental parameters of the low-speed wind tunnels. In accordance with the requirements of Annex 16 of the Convention on International Civil Aviation Organization and Part 36 of the Civil Aviation Regulations of China on noise measurement procedures, the takeoff trajectory was physically modeled; the static noise source was mapped onto the takeoff trajectory to simulate the propagation process of the noise during takeoff; and the 24 one-third-octave center frequencies that corresponded to the SPL data were corrected for geometrical dispersion, atmospheric absorption, and Doppler effects, so that the takeoff noise could be corrected to represent a real environment. In addition, the audible processing of noise data with a 110° source pointing angle was achieved, which can be useful for enabling practical observers to analyze the noise characteristics.https://www.mdpi.com/2226-4310/11/10/857open-rotor enginemixed realitynoisetakeoff trajectoryauralization |
| spellingShingle | Qing Zhang Siyi Jiang Xiaojun Yang Yongjia Xu Maosheng Zhu Noise Study Auralization of an Open-Rotor Engine open-rotor engine mixed reality noise takeoff trajectory auralization |
| title | Noise Study Auralization of an Open-Rotor Engine |
| title_full | Noise Study Auralization of an Open-Rotor Engine |
| title_fullStr | Noise Study Auralization of an Open-Rotor Engine |
| title_full_unstemmed | Noise Study Auralization of an Open-Rotor Engine |
| title_short | Noise Study Auralization of an Open-Rotor Engine |
| title_sort | noise study auralization of an open rotor engine |
| topic | open-rotor engine mixed reality noise takeoff trajectory auralization |
| url | https://www.mdpi.com/2226-4310/11/10/857 |
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