書誌事項
- タイトル別名
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- The Thermo-Aerodynamical Analysis of Combustion Gas Flow : 2nd Report, One Dimensional Theory of Annular, Combustion Chamber
- ネンショウ キリュウ ノ オンド , アツリョク オヨビ ソクド ノ ヘンカ 2
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抄録
Continued from the first report, in which the combustion gas flow throush a single chamber was analyzed, this paper presents the theory of gas flow through a typical annular combustion chamber of gas turbine or jet engine by using the thermo-aerodynamical analysis. By one numerical calculation, it was quantitatively shown that : (1) the cooling air which flows the outer space of annular combustion chamber enters naturally into the inner space throush the mixing holes by the pressure difference between outside and inside and (2) it prevents the increase of temperature of combustion gas and it promotes the increase of gas velocity, while it makes the large pressure drop by mixing in addition to that by friction and expansion.
収録刊行物
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- 日本機械学會論文集
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日本機械学會論文集 27 (174), 200-205, 1961
一般社団法人 日本機械学会
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詳細情報 詳細情報について
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- CRID
- 1390282680135153152
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- NII論文ID
- 110002351340
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- NII書誌ID
- AN00187419
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- ISSN
- 21859485
- 00290270
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- NDL書誌ID
- 9150717
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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