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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. ISAS report/Institute of Space and Aeronautical Science,University of Tokyo

Experimental Studies on Driving Mechanism of the High Frequency Combustion Oscillation in a Premixed Gas Rocket

https://jaxa.repo.nii.ac.jp/records/34401
https://jaxa.repo.nii.ac.jp/records/34401
5fab3154-bda3-445b-a73b-30951f117e8b
名前 / ファイル ライセンス アクション
SA2400578.pdf SA2400578.pdf (2.9 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 Experimental Studies on Driving Mechanism of the High Frequency Combustion Oscillation in a Premixed Gas Rocket
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 TAKENO, Tadao

× TAKENO, Tadao

en TAKENO, Tadao

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出版者
出版者 東京大学宇宙航空研究所
出版者(英)
出版者 Institute of Space and Aeronautical Science,University of Tokyo
書誌情報 en : ISAS report/Institute of Space and Aeronautical Science,University of Tokyo

巻 33, 号 2, p. 41-72, 発行日 1968-01
抄録(英)
内容記述タイプ Other
内容記述 The experimental studies were conducted to make clear the initiating and driving mechanism of the longitudinal high frequency combustion oscillation in a rocket motor burning a premixed gas as the propellant. The effects of several variables upon the critical oscillation period, which has been found in the previous studies to govern the occurrence of the oscillation, were studied in the beginning. Then the distribution of the gas temperature in the reaction zone during the oscillation was measured in detail. Finally, the photographic study of the reaction zone during the oscillation as well as during the steady combustion was made by the high speed schlieren motion picture. The results have made clear that the shock wave theory in which the driving mechanism depends on chemical kinetic factors is invalid for describing the occurrence of the oscillation. The interaction between the pressure wave and the combustion process which provides the driving force of the oscillation was found to be of a rather complicated fluid-mechanical nature. The shock wave plays no important role in this interaction. The characteristic time which governs the occurrence of the oscillation was identified with the ignition time delay of the unburnt propellant in the hot combustion gas stream. The latter was found to be of a chemical nature depending chiefly upon the propellant equivalence ratio, although some small effects of the combustion chamber pressure and the injection Mach number of the propellant were found in the experiments.
ISSN
収録物識別子タイプ ISSN
収録物識別子 0372-1418
書誌レコードID
収録物識別子タイプ NCID
収録物識別子 AA00675986
資料番号
内容記述タイプ Other
内容記述 資料番号: SA2400578000
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