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JAXA極超音速風洞で用いている気体モデル
https://jaxa.repo.nii.ac.jp/records/5839
https://jaxa.repo.nii.ac.jp/records/58396d1e6a54-e2bd-43dc-94b9-4d9b49464a50
名前 / ファイル | ライセンス | アクション |
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63330004.pdf (1.1 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 | JAXA極超音速風洞で用いている気体モデル | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 極超音速風洞 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 気体モデル | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 理想気体 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 風洞試験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | マッハ数 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 空気力 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | よどみ点圧力 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 極超音速流 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | よどみ点温度 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | hypersonic wind tunnel | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | air model | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | ideal gas | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wind tunnel test | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Mach number | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aerodynamic force | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | stagnation pressure | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | hypersonic flow | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | stagnation temperature | |||||
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 | Air models used in the JAXA hypersonic wind tunnels | |||||
著者 |
渡利, 實
× 渡利, 實× Watari, Minoru |
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著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 風洞技術開発センター | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Wind Tunnel Technology Center, Institute of Aerospace Technology | ||||||
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76回風洞研究会議論文集 en : JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 76th Meeting 巻 JAXA-SP-06-020, p. 23-26, 発行日 2007-03-30 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Three air models are used in JAXA hypersonic wind tunnel. They are 'perfect', 'thermally perfect', and 'real' models. Thermally perfect model considers an atomic-vibration energy. Real model considers an atomic vibration and an inter-molecular potential energy. The three models were comparatively investigated by program codes. It revealed that thermally perfect or real model has to be used in a precise analysis in hypersonic calculations. | |||||
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: AA0063330004 | |||||
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-06-020 |