Sensitive Parameters of Dynamic Excitation on Fuze Airflow-Induced Acoustic Generator
This paper aims at the power generation requirements of the fuze airflow-induced acoustic generator, analyzes the influence of structural parameters on the fluid power sound source, which is related to the power generation performance and use performance of the generator. In this paper, the orthogon...
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| Format: | Article |
| Language: | English |
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MDPI AG
2021-08-01
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| Series: | Micromachines |
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| Online Access: | https://www.mdpi.com/2072-666X/12/9/1033 |
| _version_ | 1797518181651185664 |
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| author | Zhipeng Li Jinghao Li Hejuan Chen |
| author_facet | Zhipeng Li Jinghao Li Hejuan Chen |
| author_sort | Zhipeng Li |
| collection | DOAJ |
| description | This paper aims at the power generation requirements of the fuze airflow-induced acoustic generator, analyzes the influence of structural parameters on the fluid power sound source, which is related to the power generation performance and use performance of the generator. In this paper, the orthogonal experiment method is used to study the sensitive parameters that control fluid dynamic sound sources. The results show that the annulus, the confronting distance, and cavity length can all have an impact on the sound pressure amplitude, and the sound pressure amplitude is most sensitive to the change of the confronting distance. However, the length of the resonant cavity has the most significant effect on the sound pressure frequency. The size of the annulus has a weak effect on the sound pressure frequency, and the confronting distance has almost no effect on the sound pressure frequency. The optimal combination scheme with the highest output power is selected according to the sensitive parameters. In addition, the empirical formula for the vibration frequency of the airflow-induced acoustic generator in the short resonant cavity was revised, and the influence of the annular gap on the vibration frequency was added, and the influence factor <i>α</i> = 0.3 was determined. The corrected frequency empirical formula has the smallest error between the theoretical value and the experimental value, and can be used as an effective method for estimating the vibration frequency. This provides a reference for the engineering design of the fuze airflow-induced acoustic generator, which has high military value and application prospects. |
| first_indexed | 2024-03-10T07:26:33Z |
| format | Article |
| id | doaj.art-e1b39e109a4e4c9c8f51e787ff687730 |
| institution | Directory Open Access Journal |
| issn | 2072-666X |
| language | English |
| last_indexed | 2024-03-10T07:26:33Z |
| publishDate | 2021-08-01 |
| publisher | MDPI AG |
| record_format | Article |
| series | Micromachines |
| spelling | doaj.art-e1b39e109a4e4c9c8f51e787ff6877302023-11-22T14:15:34ZengMDPI AGMicromachines2072-666X2021-08-01129103310.3390/mi12091033Sensitive Parameters of Dynamic Excitation on Fuze Airflow-Induced Acoustic GeneratorZhipeng Li0Jinghao Li1Hejuan Chen2School of Mechanical Engineering, Nanjing University of Science and Technology, Nanjing 210094, ChinaSchool of Mechanical Engineering, Nanjing University of Science and Technology, Nanjing 210094, ChinaSchool of Mechanical Engineering, Nanjing University of Science and Technology, Nanjing 210094, ChinaThis paper aims at the power generation requirements of the fuze airflow-induced acoustic generator, analyzes the influence of structural parameters on the fluid power sound source, which is related to the power generation performance and use performance of the generator. In this paper, the orthogonal experiment method is used to study the sensitive parameters that control fluid dynamic sound sources. The results show that the annulus, the confronting distance, and cavity length can all have an impact on the sound pressure amplitude, and the sound pressure amplitude is most sensitive to the change of the confronting distance. However, the length of the resonant cavity has the most significant effect on the sound pressure frequency. The size of the annulus has a weak effect on the sound pressure frequency, and the confronting distance has almost no effect on the sound pressure frequency. The optimal combination scheme with the highest output power is selected according to the sensitive parameters. In addition, the empirical formula for the vibration frequency of the airflow-induced acoustic generator in the short resonant cavity was revised, and the influence of the annular gap on the vibration frequency was added, and the influence factor <i>α</i> = 0.3 was determined. The corrected frequency empirical formula has the smallest error between the theoretical value and the experimental value, and can be used as an effective method for estimating the vibration frequency. This provides a reference for the engineering design of the fuze airflow-induced acoustic generator, which has high military value and application prospects.https://www.mdpi.com/2072-666X/12/9/1033airflow-induced acoustic generatorfluid dynamic sound sourceorthogonal testsound pressure frequency |
| spellingShingle | Zhipeng Li Jinghao Li Hejuan Chen Sensitive Parameters of Dynamic Excitation on Fuze Airflow-Induced Acoustic Generator Micromachines airflow-induced acoustic generator fluid dynamic sound source orthogonal test sound pressure frequency |
| title | Sensitive Parameters of Dynamic Excitation on Fuze Airflow-Induced Acoustic Generator |
| title_full | Sensitive Parameters of Dynamic Excitation on Fuze Airflow-Induced Acoustic Generator |
| title_fullStr | Sensitive Parameters of Dynamic Excitation on Fuze Airflow-Induced Acoustic Generator |
| title_full_unstemmed | Sensitive Parameters of Dynamic Excitation on Fuze Airflow-Induced Acoustic Generator |
| title_short | Sensitive Parameters of Dynamic Excitation on Fuze Airflow-Induced Acoustic Generator |
| title_sort | sensitive parameters of dynamic excitation on fuze airflow induced acoustic generator |
| topic | airflow-induced acoustic generator fluid dynamic sound source orthogonal test sound pressure frequency |
| url | https://www.mdpi.com/2072-666X/12/9/1033 |
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