書誌事項
- タイトル別名
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- Optimization of the Fuel Injector for the Supersonic Combustor Using a Multi Objective Genetic Algorithm
- タモクテキ イデンテキ アルゴリズム オ モチイタ チョウオンソク ネンショウキ ネンリョウ フンシャグチ ケイジョウ ノ サイテキカ
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抄録
The optimal fuel injector shape for a supersonic combustor is investigated in terms of rapid mixing of fuel jet and supersonic airstream. A Multi-Objective Genetic Algorithm (MOGA) has been applied to discover the optimal fuel injector shape, and two goals of the optimization are adopted. One is to maximize the jet core height, and the other is to minimize the total pressure loss. The algorithm works well, and the characteristics of the optimized shapes for the fuel injector are understood. The effects of the fuel injector shape, which is derived from the statistical process of the optimized shape, are numerically investigated on the jet core height and total pressure loss.
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 51 (591), 169-174, 2003
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
- 1390282679446032512
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- NII論文ID
- 130000146761
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- NII書誌ID
- AA11307372
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- ISSN
- 24323691
- 13446460
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- NDL書誌ID
- 6559608
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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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- 抄録ライセンスフラグ
- 使用不可
