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Japan Aerospace Exploration Agency Studies for the Second High-Lift Prediction Workshop
https://jaxa.repo.nii.ac.jp/records/22624
https://jaxa.repo.nii.ac.jp/records/2262439470dc2-784a-4eb7-8144-a6400894e68f
Item type | 学術雑誌論文 / Journal Article(1) | |||||
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公開日 | 2015-10-16 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Japan Aerospace Exploration Agency Studies for the Second High-Lift Prediction Workshop | |||||
言語 | ||||||
言語 | eng | |||||
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 | |||||
著者 |
村山, 光宏
× 村山, 光宏× 山本, 一臣× 伊藤, 靖× 平井, 享× 田中, 健太郎× Murayama, Mitsuhiro× Yamamoto, Kazuomi× Ito, Yasushi× Hirai, Tohru× Tanaka, Kentaro |
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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 | ||||||
株式会社菱友システムズ | ||||||
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 | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Ryoyu Systems Company, Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Ryoyu Systems Company, Ltd. | ||||||
出版者(英) | ||||||
出版者 | American Institute of Aeronautics and Astronautics | |||||
書誌情報 |
en : Journal of Aircraft 巻 52, 号 4, p. 1026-1041, 発行日 2015-07 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | This paper summarizes Japan Aerospace Exploration Agency studies using a structured grid solver UPACS and an unstructured grid solver TAS-code for the second AIAA CFD High-Lift Prediction Workshop test cases and follow-on problems. Computations are performed for the grid convergence study using the configuration without any slat tracks and flap track fairings on a series of multi-block structured grids and a series of unstructured grids provided by the High Lift Prediction Workshop committee. In this paper, the following are mainly discussed: 1) grid convergence verification study of the turbulence models using a two-dimensional bump case, 2) grid convergence studies for Spalart-Allmaras and shear stress transport turbulence models using UPACS, 3) change of grid convergence and predicted flow fields with and without a nonlinear quadratic constitutive relation model for Spalart-Allmaras and shear stress transport turbulence models using UPACS including evaluation at higher angles of attack, and 4) comparison studies using different solvers UPACS and TAS on different grid systems with and without the quadratic constitutive relation model for the Spalart-Allmaras model. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0021-8669 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA00692384 | |||||
DOI | ||||||
識別子タイプ | DOI | |||||
関連識別子 | http://dx.doi.org/10.2514/1.C033158 | |||||
関連名称 | info:doi/10.2514/1.C033158 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: PA1520039000 |