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実在気体効果をともなう極超音速流解析の検証
https://jaxa.repo.nii.ac.jp/records/36872
https://jaxa.repo.nii.ac.jp/records/368726c90d076-908e-4f21-9195-389b7918cf70
名前 / ファイル | ライセンス | アクション |
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nalsp0034013.pdf (621.3 kB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 実在気体効果をともなう極超音速流解析の検証 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 実在気体効果 | |||||
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 | 化学平衡 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 衝撃風洞 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 流れ解析システム | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | マルチブロック格子 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 翼胴模型 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 有限体積法 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | TVD風上スキーム | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | total variation diminishing | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | よどみ点 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 衝撃波干渉 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 凍結流 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 空力加熱 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ナビエ・ストークス解析システム | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | real gas effect | |||||
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 | chemical equilibrium | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | shock tunnel | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flow analysis system | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | multi block grid | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wing body model | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | finite volume method | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | TVD upwind scheme | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | total variation diminishing | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | stagnation point | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | shock wave interaction | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | frozen flow | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aerodynamic heating | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Navier Stokes analysis system | |||||
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 | Validation of the computation of hypersonic flow with real gas effects | |||||
著者 |
岸本, 琢司
× 岸本, 琢司× 花光, 明× 尾藤, 日出夫× Kishimoto, Takuji× Hanamitsu, Akira× Bito, Hideo |
|||||
著者所属 | ||||||
川崎重工業 航空宇宙事業本部 | ||||||
著者所属 | ||||||
川崎重工業 航空宇宙事業本部 | ||||||
著者所属 | ||||||
宇宙開発事業団 | ||||||
著者所属(英) | ||||||
en | ||||||
Kawasaki Heavy Industries Ltd Space Project Engineering Department | ||||||
著者所属(英) | ||||||
en | ||||||
Kawasaki Heavy Industries Ltd Space Project Engineering Department | ||||||
著者所属(英) | ||||||
en | ||||||
National Space Development Agency of Japan | ||||||
出版者 | ||||||
出版者 | 航空宇宙技術研究所 | |||||
出版者(英) | ||||||
出版者 | National Aerospace Laboratory (NAL) | |||||
書誌情報 |
航空宇宙技術研究所特別資料 en : Special Publication of National Aerospace Laboratory 巻 34, p. 67-72, 発行日 1997-01 |
|||||
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 | 航空宇宙技術研究所 6-7 JUN. 1996 東京 日本 | |||||
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 | National Aerospace Laboratory 6-7 JUN. 1996 Tokyo Japan | |||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 化学平衡であると推定される実在気体効果をともなう極超音速流の数値解析を、HEG(ゲッチンゲン高エンタルピー風洞)衝撃風洞試験データとの比較により検証した。流れ解析システムはマルチブロック型構造格子を用い、化学平衡実在気体効果の評価のための曲線あてはめ法による有限体積TVD(Total Variation Diminishing)風上スキームに基づいている。球まわりと単純翼胴模型まわりのそれぞれの流れを計算した。球まわりの流れの数値結果は、よどみ点における熱流束を考えると衝撃風洞試験データと非常によく一致した。単純翼胴模型の結果は衝撃波・衝撃波干渉による位置と熱流束ピーク値に関する実在気体効果を考慮することによって、凍結流の結果と比較して定性的に向上した。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The validation of the computation of hypersonic flow with real gas effects, that is assumed to be chemical equilibrium, have been carried out by the comparison with the HEG (High Enthalpy shock tunnel in Goettingen) shock tunnel test data. The flow analysis system uses a structured multi-block grid, and is based on finite volume TVD (Total Variation Diminishing) upwind scheme with the curve fitting to estimate chemical equilibrium real gas effects. Calculations were done to the flows around a sphere and the simple wing-body model respectively. The numerical results of the flow around a sphere showed very good agreement with the shock tunnel test data in the view of heat flux at a stagnation point. The results of the simple wing-body model were qualitatively improved by taking account of real gas effects with respect to the location and value of peak heat flux by shock-shock interaction, compared with frozen flow results. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0289-260X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN10097345 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0000685013 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: NAL SP-34 |