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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 in the Laminar Boundary Layer on a Porous Flat Plate with Hot Gas Injection

https://jaxa.repo.nii.ac.jp/records/34612
https://jaxa.repo.nii.ac.jp/records/34612
4197ddb4-debe-404e-9976-7a0f772e73d3
名前 / ファイル ライセンス アクション
SA2404869.pdf SA2404869.pdf (1.2 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 in the Laminar Boundary Layer on a Porous Flat Plate with Hot Gas Injection
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 27, 号 5, p. 139-155, 発行日 1961-05
抄録(英)
内容記述タイプ Other
内容記述 In the present paper, an analysis is made on the problem of ignition and flame stabilization of the steady stream of combustible gaseous mixtures in the laminar boundary layer on a porous flat plate, from the surface of which hot inert gases or combustion products are injected into the boundary layer, and the effect of hot gas injection on ignition and flame stabilization in the boundary layer is examined. A one-step unopposed global reaction following any order reaction kinetics with temperature dependence according to the Arrhenius rate law is assumed. The boundary layer equations of aerothermochemistry are solved for the special case where ν_ω(χ)&prop;√<μ∞/χ> by the iterative method and the general analytic solutions of N'th approximation to the temperature and concentration profiles across the boundary layer are presented. These analytic results are then applied to the problem of the thermal decomposition of azomethane and numerical calculations are carried out for the first-order approximation. It is found that the effects of hot gas injection on the ignition and flame stabilization in the boundary layer are remarkable and the characteristic stay time decreases monotonously with the increase of injection rate. This is due to the fact that the temperature profile in the case without chemical reaction (i.e.x=0) approaches the separation-type profile as the injection rate increases.
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: SA2404869000
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