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  1. コンテンツタイプ
  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. The Institute of Space and Astronautical Science report

Gas-Particle Mixture Flows in a Spinning Solid Rocket Motor

https://jaxa.repo.nii.ac.jp/records/31370
https://jaxa.repo.nii.ac.jp/records/31370
58391749-6192-43a5-a35d-ccd50c970021
名前 / ファイル ライセンス アクション
SA0034946.pdf SA0034946.pdf (801.5 kB)
Item type 紀要論文 / Departmental Bulletin Paper(1)
公開日 2015-03-26
タイトル
タイトル Gas-Particle Mixture Flows in a Spinning Solid Rocket Motor
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 YAMAMOTO, Masaya

× YAMAMOTO, Masaya

en YAMAMOTO, Masaya

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OGUCHI, Hakuro

× OGUCHI, Hakuro

en OGUCHI, Hakuro

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出版者
出版者 宇宙科学研究所
出版者(英)
出版者 Institute of Space and Astronautical Science
書誌情報 en : The Institute of Space and Astronautical Science report

巻 607, p. 1-15, 発行日 1983-09
抄録(英)
内容記述タイプ Other
内容記述 Main aim of this studiy is to clarify the spin stabilization effect on the flow field. Internal flow field of the solid rocket motor is numerically analyzed by the time-dependent finite difference method in combination with the boundary-fitted curvilinear coordinate technique. Computation was carried out about flow through the nozzle with cigarette-burn type chamber and also with spherical chamber. The thrust performance and the behavior of the particle impingement upon nozzle wall were analyzed. As the results, the followings are shown, (1) The thrust loss caused by two-phase flow is less for the nozzle with cigarette-burn type chamber, than for the nozzle with spherical chamber. (2) As to the nozzle with cigarette-burn type chamber, the thrust loss of 2 to 3 percent occurs under the 2 r.p.s. spin stabilization. In no-spin case, particle impingement is not observed over a whole nozzle wall, while in the case of spin stabilization it is observed on the nozzle wall near the exit. (3) As to the nozzle with spherical chamber, there is no appreciable effect of the spin stabilization.
ISSN
収録物識別子タイプ ISSN
収録物識別子 0285-6808
書誌レコードID
収録物識別子タイプ NCID
収録物識別子 AA10632072
資料番号
内容記述タイプ Other
内容記述 資料番号: SA0034946000
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