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障害物励起音の特性に関する実験的数値的検討
https://jaxa.repo.nii.ac.jp/records/4708
https://jaxa.repo.nii.ac.jp/records/47088c28080c-a7b8-4175-b700-94953aee4ed0
名前 / ファイル | ライセンス | アクション |
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64967001.pdf (1.3 MB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 障害物励起音の特性に関する実験的数値的検討 | |||||
言語 | ||||||
言語 | jpn | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_5794 | |||||
資源タイプ | conference paper | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Experimental and Numerical Study of Excited Sound from a block | |||||
著者 |
蔵居, 慧之
× 蔵居, 慧之× 白石, 裕之× Kurai, Satoshi× Shiraishi, Hiroyuki |
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著者所属 | ||||||
大同大学 | ||||||
著者所属 | ||||||
大同大学 | ||||||
著者所属(英) | ||||||
en | ||||||
Daido University | ||||||
著者所属(英) | ||||||
en | ||||||
Daido University | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構 | |||||
出版者(英) | ||||||
出版者 | Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙航空研究開発機構特別資料: 第42回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2010 論文集 en : JAXA Special Publication: Proceedings of 42nd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2010 巻 JAXA-SP-10-012, 発行日 2011-02-28 |
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会議概要(会議名, 開催地, 会期, 主催者等) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 第42回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2010(2010年6月24日-25日, 米子コンベンションセンター BiG SHiP) | |||||
会議概要(会議名, 開催地, 会期, 主催者等)(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 42nd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2010 (June 24-25, 2010. Yonago Convention Center BiG SHiP), Yonago, Tottori Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Though edge tone and aeolian tone are both treated as excited sounds from blocks, they are often to be done by different approaches to numerical analyses because an edge tone only has feedback loop caused by sound waves. In experimental apparatus, however, these phenomena can be generated simultaneously. Therefore, we have constructed the new soundproof room made by sound arresting walls considering of TV studio, in order to study the transition from edge tone to aeolian tone. As a numerical approach, Finite Difference Lattice Boltzmann Method (FDLBM), which is authorized as generalized numerical analysis, is also applied for evaluating the effect of the gas species in the transition. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: カラー図版あり | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-113X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11984031 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0064967001 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JAXA-SP-10-012 |