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  2. 紀要論文 (Departmental Bulletin Paper)
  1. 機関資料(JAXA, former ISAS, NAL, NASDA)
  2. 旧機関資料 (JAXA, former-ISAS, NAL, NASDA)
  3. 宇宙科学研究所: ISAS Report等を含む (former ISAS (The Institute of Space and Astronautical Science): Including ISAS Report etc.)
  4. Report/Aeronautical Research Institute, University of Tokyo

Ignition and Flame Stabilization of Stream of Combustible Gaseous Mixtures by Hot Jet

https://jaxa.repo.nii.ac.jp/records/34604
https://jaxa.repo.nii.ac.jp/records/34604
69d87c0b-01e8-4741-9c3b-3f7e5b73b7c7
名前 / ファイル ライセンス アクション
SA2404845.pdf SA2404845.pdf (1.1 MB)
Item type 紀要論文 / Departmental Bulletin Paper(1)
公開日 2015-03-26
タイトル
タイトル Ignition and Flame Stabilization of Stream of Combustible Gaseous Mixtures by Hot Jet
言語 en
言語
言語 eng
資源タイプ
資源タイプ識別子 http://purl.org/coar/resource_type/c_6501
資源タイプ departmental bulletin paper
著者 TSUJI, Hiroshi

× TSUJI, Hiroshi

en TSUJI, Hiroshi

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出版者
出版者 東京大学航空研究所
出版者(英)
出版者 Aeronautical Research Institute, University of Tokyo
書誌情報 東京大學航空研究所報告
en : Report/Aeronautical Research Institute, University of Tokyo

巻 26, 号 8, p. 119-136, 発行日 1960-06
抄録(英)
内容記述タイプ Other
内容記述 The ignition and flame stabilization of the flowing combustible gaseous mixtures by a hot jet of combustion products or inert gases are important phenomena in many apparatus, such as ramjet burners or rocket combustion chambers. In the present paper, the problem of the ignition of the combustible gaseous stream by a hot jet is formulated and analyzed, considering a simplified model and using the boundary layer approximation of aerothermochemistry. A one-step unopposed global reaction following any order reaction kinetics with temperature dependence according to the Arrhenius rate law is assumed. The Prandtl and Schmidt numbers are assumed to be equal, then a similarity between the equation of energy and the diffusion equation exists, greatly simplifying the analysis. Approximate but general analytic expressions for the N'th approximation to the temperature and concentration profiles are obtained. These analytic results are applied to the problems of the thermal decomposition of azomethane and the thermal decomposition of hydrazine. Numerical calculations are carried out for the first-order approximation. It is confirmed that if the width of the jet is large enough, then the ignition always takes place at some point of the stream, but if the width of the jet is small, whether or not the ignition takes place depends on the width of the jet and the temperature of the hot gas.
ISSN
収録物識別子タイプ ISSN
収録物識別子 0376-1061
書誌レコードID
収録物識別子タイプ NCID
収録物識別子 AA00514444
資料番号
内容記述タイプ Other
内容記述 資料番号: SA2404845000
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