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Development of an advanced multi-material bird-strike model using the smoothed particle hydrodynamics method
https://jaxa.repo.nii.ac.jp/records/22461
https://jaxa.repo.nii.ac.jp/records/224611f1b2475-0e81-4cc9-a28b-03e21451c44d
Item type | 学術雑誌論文 / Journal Article(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Development of an advanced multi-material bird-strike model using the smoothed particle hydrodynamics method | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | bird-strike | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | certification | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | hydrodynamic | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | multi-material | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | SPH | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | gelatine | |||||
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 | |||||
アクセス権 | ||||||
アクセス権 | metadata only access | |||||
アクセス権URI | http://purl.org/coar/access_right/c_14cb | |||||
その他のタイトル | ||||||
その他のタイトル | SPH法を用いた先進多材料鳥衝突モデルの開発 | |||||
著者 |
McCallum, Stuart
× McCallum, Stuart× 少路, 宏和× 秋山, 弘行× McCallum, Stuart× Shoji, Hirokazu× Akiyama, Hiroyuki |
|||||
著者所属 | ||||||
宇宙航空研究開発機構航空本部(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構航空本部(JAXA) | ||||||
著者所属 | ||||||
株式会社菱友システムズ | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Ryoyu Systems Co., Ltd. | ||||||
出版者(英) | ||||||
出版者 | Taylor & Francis | |||||
書誌情報 |
en : International Journal of Crashworthiness 巻 18, 号 6, p. 579-597, 発行日 2013-10-17 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | This paper presents the results of simulations used to verify the smoothed particle hydrodynamics method for bird-strike simulation and assess the influence of the bird-model shape, internal organ structure and certification configurations by comparing traditional primitive models to a new model based on biometric and published CT-scan data. Initially, a series of analyses and sensitivity studies are performed for traditional models with air porosity which show the Hugoniot pressure, steady-state pressure, impulse and force history data are in close agreement with classical hydrodynamic theory. The new model which includes eight body parts and accounts for variations in density and material strength indicates a lower Hugoniot pressure and increased asymmetry during impact. The results of the new model also show that a bird in a representative flight configuration has a longer impact duration and higher peak impact force when compared to the current folded configuration used in certification testing and simulations. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1358-8265 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA1164914X | |||||
DOI | ||||||
識別子タイプ | DOI | |||||
関連識別子 | http://dx.doi.org/10.1080/13588265.2013.843498 | |||||
関連名称 | info:doi/10.1080/13588265.2013.843498 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: PA1420008000 |