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航空機の脚要素と脚収納部の干渉による騒音発生の基礎検討
https://jaxa.repo.nii.ac.jp/records/47346
https://jaxa.repo.nii.ac.jp/records/473464302c56f-cf18-4072-b195-a9fa270ce529
名前 / ファイル | ライセンス | アクション |
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AA2030013025.pdf (4.0 MB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2021-02-08 | |||||
タイトル | ||||||
タイトル | 航空機の脚要素と脚収納部の干渉による騒音発生の基礎検討 | |||||
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 | Basic Investigation on Noise Generation Due to Interactions between Aircraft Landing Gear Components and Gear Bay | |||||
著者 |
山本, 一臣
× 山本, 一臣× 梁, 裕卓× 村山, 光宏× 野崎, 理× 平井, 亨× YAMAMOTO, Kazuomi× YAN, Yutaku× MURAYAMA, Mitsuhiro× NOZAKI, Osamu× HIRAI, Toru |
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著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
スカイマーク株式会社 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
高知工科大学 | ||||||
著者所属 | ||||||
株式会社菱友システムズ | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Skymark Airlines inc. | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Kochi University of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Ryoyu Systems Co., Ltd. | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構(JAXA) | |||||
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: 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2020オンライン論文集 en : JAXA Special Publication: Proceedings of Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2020 Online 巻 JAXA-SP-20-008, p. 191-198, 発行日 2021-02-08 |
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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 | 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2020オンライン (2020年9月28日-30日. 日本航空宇宙学会 : 宇宙航空研究開発機構(JAXA)オンライン会議) | |||||
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 | Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2020 Online (September 28-30, 2020. The Japan Society for Aeronautical and Space Sciences : Japan Aerospace Exploration Agency (JAXA), Online meeting) | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In order to understand the noise generation due to interactions between the side-brace wake and the gear-bay shear-layer of the main landing gear, a simple numerical flow analysis on a rectangular open cavity including a circular cylinder is conducted by using two-dimensional laminar flow computations. The results show that modification of the cylinder location relative to the cavity leading edge drastically changes the oscillation modes and frequency characteristics of the cavity flow. Although the computational model is too simple to clarify the interaction noise of the real aircraft landing-gear, it provides a basic knowledge of the noise generation physics. | |||||
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 | |||||
ISSNONLINE | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 2433-2232 | |||||
著者版フラグ | ||||||
出版タイプ | VoR | |||||
出版タイプResource | http://purl.org/coar/version/c_970fb48d4fbd8a85 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA2030013025 | |||||
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-20-008 |