書誌事項
- タイトル別名
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- Experiments of Supersonic Mixing and Combustion Enhancement Using Alternating-Wedge Strut: Part 1 —Effects of Supersonic Streamwise Vortices in a Scramjet Combustor
- 縦渦導入型燃料噴射ストラットの超音速混合燃焼実験(第1報)スクラムジェット燃焼器における超音速縦渦列の効果
- タテウズ ドウニュウガタ ネンリョウ フンシャ ストラット ノ チョウオンソク コンゴウ ネンショウ ジッケン ダイ1ポウ スクラムジェット ネンショウキ ニ オケル チョウオンソク タテ ウズレツ ノ コウカ
- Experiments of Supersonic Mixing and Combustion Enhancement Using Alternating-Wedge Strut: Part 1 —Effects of Supersonic Streamwise Vortices in a Scramjet Combustor
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Effects of streamwise vortices on enhancement of supersonic mixing and combustion are examined in a scramjet combustor whose main flow is a Mach 2.45 vitiation air stream with a total temperature of 2200K. The fuel injector strut called “Alternating-Wedge Strut (AW-Strut)” is used to generate streamwise vortices and to inject hydrogen fuel into their core region. For comparison, a generic strut, “MO-Strut,” without streamwise vortex generation is also examined. Direct visualization of flame shows rapid formation of streamwise vortices and ignition/combustion within the vortices already upstream of the strut trailing edge. Wall pressure measurements along the combustor show that for the case of AW-Strut the wall pressure rise due to combustion is almost twice that of the MO-Strut case. Gas sampling at the combustor exit demonstrates that much more uniform fuel/air mixing is obtained for the case of AW-Strut. The present results verify the phenomenal performance of the supersonic streamwise vortices for enhancement of supersonic mixing and combustion.
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 50 (579), 135-135, 2002
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
- 1390282679447397120
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- NII論文ID
- 10007976900
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- NII書誌ID
- AA11307372
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- ISSN
- 24323691
- 13446460
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- NDL書誌ID
- 6138586
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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
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- 使用不可