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Standard Dynamics Model における空力微係数の定常・非定常解析
https://jaxa.repo.nii.ac.jp/records/4278
https://jaxa.repo.nii.ac.jp/records/42783fcc5c7c-6e10-4551-b631-a212c7b647b4
名前 / ファイル | ライセンス | アクション |
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61958038.pdf (1.2 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 | Standard Dynamics Model における空力微係数の定常・非定常解析 | |||||
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 | Steady/Unsteady Analysis of Aerodynamic Derivatives on Standard Dynamics Model | |||||
著者 |
橋本, 敦
× 橋本, 敦× 橋爪, 幹人× 砂田, 茂× 村上, 桂一× 上野, 真× Hashimoto, Atsushi× Hashizume, Mikihito× Sunada, Shigeru× Murakami, Keiichi× Ueno, Makoto |
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著者所属 | ||||||
宇宙航空研究開発機構航空本部数値解析技術研究グループ(JAXA) | ||||||
著者所属 | ||||||
大阪府立大学 | ||||||
著者所属 | ||||||
大阪府立大学 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構航空本部数値解析技術研究グループ(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構航空本部風洞技術開発センター(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Numerical Simulation Research Group, Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Osaka Prefecture University | ||||||
著者所属(英) | ||||||
en | ||||||
Osaka Prefecture University | ||||||
著者所属(英) | ||||||
en | ||||||
Numerical Simulation Research Group, Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Wind Tunnel Technology Center, Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA) | ||||||
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 en : JAXA Special Publication: Proceedings of 44th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2012 巻 JAXA-SP-12-010, p. 225-230, 発行日 2013-03-29 |
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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44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2012 (2012年7月5日-6日. 富山国際会議場大手町フォーラム), 富山市, 富山県 | |||||
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 | 44th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2012 (July 5-6, 2012. Toyama International Conference Center), Toyama Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Standard Dynamics Model (SDM) is computed to validate the prediction of dynamics derivatives using grid generator “HexaGrid” and flow solver “FaSTAR”. The static and dynamic derivatives are computed at M=0.6, Re=2.31×10(exp 6), α=0-20deg. The forced oscillation method is employed to compute the dynamic derivatives. The effects of local time step and number of inner iteration are investigated. The computed results show good agreement with wind tunnel data. It is found that we have to evaluate the dynamic derivatives of SDM using unsteady simulation since the effects of Czα and Cmα are rather large, and these are not considered in the steady simulation. | |||||
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: AA0061958038 | |||||
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-12-010 |