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宇宙機音響振動応答予測に関するFEA-SEA統合法適用の理論検討と実験検証
https://jaxa.repo.nii.ac.jp/records/22422
https://jaxa.repo.nii.ac.jp/records/22422173838a0-d7cd-4446-a4ee-32565624ef78
名前 / ファイル | ライセンス | アクション |
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PA1410058.pdf (829.0 kB)
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Item type | 学術雑誌論文 / Journal Article(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 宇宙機音響振動応答予測に関するFEA-SEA統合法適用の理論検討と実験検証 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Acoustic; Statistical Energy Analysis; Random Vibration; Space Engineering; Joint Acceptance; FEA; Diffuse Sound Field | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_6501 | |||||
資源タイプ | journal article | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Theory Review and Test Verification about Combination of FEA and SEA Methods to Predict the Vibroacoustic Response of Spacecraft Structure | |||||
著者 |
赤城, 弘樹
× 赤城, 弘樹× 安藤, 成将× 柳瀬, 恵一× 施勤, 忠× Akagi, Hiroki× Ando, Shigemasa× Yanagase, Keiichi× Shi, Qinzhong |
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著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency(JAXA) | ||||||
出版者 | ||||||
出版者 | 日本機械学会 | |||||
書誌情報 |
日本機械学會論文集 C編 巻 79, 号 802, p. 1960-1969, 発行日 2013-06 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Spacecraft is exposed to the severe random vibration by acoustic during its launch. In the spacecraft design, random vibration of spacecraft components mounted on panel structure during launch environments needs to be predicted. In the present methods, SEA is the method for analyzing the high frequency band, FEA is for the low frequency band. This paper applies combination of FEA and SEA methods to predict the vibroacoustic response of spacecraft structure which may be extended to wide frequency range experienced during the launch. The combination methods focuses on the vibroacoustic prediction which keeps advantages to use detail model of structure expressed by FEA and statistical energy approach expressed by SEA of reverberant acoustic excitation. The combination method is applied to diffuse sound field excitation of honeycomb panel, and is compared with acoustic excitation test and the results from conventional approach of BEM ,joint acceptance and SEA. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0387-5024 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN00187463 | |||||
DOI | ||||||
関連タイプ | isVersionOf | |||||
識別子タイプ | DOI | |||||
関連識別子 | http://dx.doi.org/10.1299/kikaic.79.1960 | |||||
関連名称 | info:doi/10.1299/kikaic.79.1960 | |||||
権利 | ||||||
権利情報 | (C)2013 日本機械学会 | |||||
著者版フラグ | ||||||
出版タイプ | AM | |||||
出版タイプResource | http://purl.org/coar/version/c_ab4af688f83e57aa | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: PA1410058000 |