1.

図書

図書
Mark M. Meerschaert著 ; 佐藤一憲 [ほか] 訳
出版情報: 東京 : 共立出版, 2015.1
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2.

図書

図書
中曽根祐司編著 ; 田中純夫 [ほか] 共著
出版情報: 東京 : コロナ社, 2014.4
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3.

図書

図書
F. ジョン著 ; 佐々木徹, 示野信一, 橋本義武訳
出版情報: 東京 : 丸善出版, 2012.3
シリーズ名: シュプリンガー数学クラシックス ; 第12巻
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4.

論文

論文
佐々木, 徹 ; 天野, 俊輔 ; 渡辺, 哲也 ; 古畑, 朋彦 ; 新井, 雅隆
出版情報: 日本機械学會論文集. B編.  74  pp.957-964,  2008-05-25.  日本機械学会
概要: application/pdf<br />Journal Article<br />A low NO_x combustor for kerosene-fueled micro gas turbine based on a new concept was proposed. The combustor consisted of primary and secondary combustion zones, and they were connected by a throat. A swirler was set between the primary and secondary combustion zones. In order to enhance recirculation of burned gas in the primary combustion zone, combustion air was introduced through the swirler and forced to flow upward to the combustor bottom. In this study, fundamental combustion characteristics such as lean combustion limit, exhaust gas composition and combustion gas temperature were measured using three fuel atomizers which rated flow rates were 3.0 gallon/h, 4.5 gallon/h and 6.0 gallon/h respectively. It was shown that the combustion stability and emission characteristics in the case of 3.0 gallon/h nozzle were superior to those in other cases. Further, gas velocity in the primary combustion zone was measured by Leaser Doppler Anemometer (LDA) and behavior of the recirculation of burned gas was investigated 続きを見る
5.

論文

論文
佐々木, 徹 ; 天野, 俊輔 ; 渡辺, 哲也 ; 世取山, 幸作 ; 古畑, 朋彦 ; 新井, 雅隆
出版情報: 日本機械学會論文集. B編.  74  pp.965-972,  2008-04-25.  日本機械学会
概要: application/pdf<br />Journal Article<br />A low NO_x combustor for kerosene-fueled micro gas turbine based on a new concept was proposed. The combustor consisted of primary and secondary combustion zones, and they were connected by a throat. A swirler was set between the primary and secondary combustion zones. In order to enhance recirculation of burned gas in the primary combustion zone, combustion air was introduced through the swirler and forced to flow upward to the combustor bottom. In this study, effects of configuration of primary combustion zone on combustion gas flow in it were investigated. The length of primary combustion zone, swirler vane angle, diameter of throat and height of guide vane were changed independently from the standard configuration. Distributions of gas flow in the primary combustion zone were measured with LDA. The relation between combustion stability and the distributions of gas flow was discussed, and it was found that appropriate combustion gas recirculation in the primary combustion zone was necessary to keep combustion stability high. 続きを見る
6.

図書

図書
F. ジョン著 ; 佐々木徹, 示野信一, 橋本義武訳
出版情報: 東京 : シュプリンガー・フェアラーク東京, 2003.10
シリーズ名: シュプリンガー数学クラシックス ; 第12巻
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