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A study on heat transfer in a scramjet leading edge model
https://jaxa.repo.nii.ac.jp/records/41172
https://jaxa.repo.nii.ac.jp/records/411721a4e1ab1-f428-4c6f-a4b5-db683d93ed81
名前 / ファイル | ライセンス | アクション |
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naltr1187t.pdf (999.7 kB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | A study on heat transfer in a scramjet leading edge model | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | スクラムジェットエンジン | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 前縁加熱 | |||||
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 | 超音速流れ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 冷却構造 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 冷却パネル | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 性能試験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | アクティブクーリング | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 再生冷却 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 熱防護 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 熱流束測定 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 熱伝達 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | クロスフロー型冷却パネル | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 熱構造解析 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | NTO/MMHガス発生器 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | scramjet engine | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | leading edge heating | |||||
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 | supersonic flow | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | cooling structure | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | cooling panel | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | performance test | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | active cooling | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | regenerative cooling | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | thermal protection | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | heat flux measurement | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | heat transfer | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | crossflow type cooling panel | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | thermostructrural analysis | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | NTO/MMH gas generator | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル | ||||||
その他のタイトル | スクラムジェット前縁モデルにおける熱伝達の研究 | |||||
著者 |
植田, 修一
× 植田, 修一× 櫻中, 登× 斎藤, 俊仁× 伊藤, 勝宏× 若松, 義男× 今井, 究× Ueda, Shuichi× Sakuranaka, Noboru× Saito, Toshihito× Ito, Katsuhiro× Wakamatsu, Yoshio× Imai, Kiwamu |
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著者所属 | ||||||
航空宇宙技術研究所 角田支所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 角田支所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 角田支所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 角田支所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 角田支所 | ||||||
著者所属 | ||||||
石川島播磨重工業 | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Kakuda Research Center | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Kakuda Research Center | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Kakuda Research Center | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Kakuda Research Center | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Kakuda Research Center | ||||||
著者所属(英) | ||||||
en | ||||||
Ishikawajima-Harima Heavy Industries Co Ltd | ||||||
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報告 en : Technical Report of National Aerospace Laboratory 巻 1187T, p. 1-16, 発行日 1992-12 |
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抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | スクラムジェットエンジンのインレットやストラット前縁部を模擬した冷却構造パネルの加熱試験および解析を行なった。円弧型の前縁部を持つニッケル電鋳製の冷却パネルを超音速の高温ガス流中で加熱した。ガス発生器として、NTO(4酸化2窒素)/MMH(モノメチルヒドラジン)を酸化剤および燃料とする矩形燃焼器を使用した。ガス発生器出口の一様流マッハ数は約2.67である。冷却材として水を使用し、冷却水温の上昇から熱流束分布を測定した。2次元のCFD(計算流体力学)コードおよび有限要素法コードによる解析を行ない、実験結果と比較した。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Heating tests and analysis of a cooling panel that simulates the leading edge of the scramjet engine inlet or strut were performed using crossflow type water-cooled panel with a circular leading edge. The cooling panel was fabricated by nickel electroforming and heated by supersonic hot gas. An NTO (Nitrogen TetraOxide) and MMH (MonoMethyl Hydrazine) rectangular chamber was used as the gas generator. The free stream Mach number at the nozzle exit was about 2.67. Water was used as the coolant and heat flux distribution was measured based on the temperature increase. Thermal analysis were performed using a two-dimensional CFD (Computational Fluid Dynamics) code and a finite element code. The results of the analysis were compared with the experimental data. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0389-4010 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0004202000 | |||||
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 TR-1187T |