書誌事項
- タイトル別名
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- A Study on Reduction of Aerodynamic Heating by Opposing Jet in Supersonic Flow
- チョウオンソクリュウ チュウ ノ ギャクフンシャ ジェット ニ ヨル クウリキ カネツ テイゲン ニ カンスル ケンキュウ
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抄録
An experimental study on reduction of aerodynamic heating due to opposing jet in supersonic flow has been conducted. Experiments are conducted by using a conventional blowdown type wind tunnel. A hemisphere model is installed into supersonic free stream of Mach number of 4 and coolant gas is injected through a sonic nozzle at the top of the model. Significant decrease of surface heat flux distribution is observed and opposing jet is proved to be quite effective on the reduction of aerodynamic heating at the nose region of the blunt body. The effect of total pressure ratio of opposing jet to the free stream on the reduction of aerodynamic heating is also investigated.
収録刊行物
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- 日本航空宇宙学会論文集
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日本航空宇宙学会論文集 52 (600), 38-44, 2004
一般社団法人 日本航空宇宙学会
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詳細情報 詳細情報について
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- CRID
- 1390001204468762240
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- NII論文ID
- 10011983769
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- NII書誌ID
- AA11307372
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- ISSN
- 24323691
- 13446460
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- NDL書誌ID
- 6830166
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- 本文言語コード
- ja
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- データソース種別
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- JaLC
- NDL
- Crossref
- CiNii Articles
- KAKEN
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- 抄録ライセンスフラグ
- 使用不可