ロケットエンジン噴射器流れの数値解析

Material type: 文書・図像類

Author: 清水, 和弥ほか

Publisher: 宇宙航空研究開発機構

Publication date: 2006-01-20

Material Format: Digital

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Note (General)：: Numerical study on the jet flow in a high pressure fluid has been conducted in order to simulate atomization, mixing and combustion in a liquid rocket...

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Material Type: 文書・図像類
Title: ロケットエンジン噴射器流れの数値解析
Author/Editor: 清水, 和弥
清水, 太郎
Shimizu, Kazuya
Shimizu, Taro
Author Heading: 清水, 和弥
清水, 太郎
Shimizu, Kazuya
Shimizu, Taro
Publication, Distribution, etc.: 宇宙航空研究開発機構
Publication Date: 2006-01-20
Publication Date (W3CDTF): 2006-01-20
Alternative Title: Numerical study of rocket engine injector flow
Periodical title: 宇宙航空研究開発機構特別資料: 平成16年度総合技術研究本部宇宙領域宇宙科学研究本部合同研究成果報告書:宇宙輸送系基盤技術 = JAXA Special Publication: FY2004 Report of Joint Research Achievements of the Space Division of Institute of Aerospace Technology and Institute of Space and Astronautical Science: Basic Technologies of Space Transportation Systems
No. or year of volume/issue: JAXA-SP-05-010
Volume: JAXA-SP-05-010
Pages: 3-8
ISSN (Periodical Title): ISSN : 1349-113X
Text Language Code: jpn
Subject Heading: 数値解析
数値シミュレーション
噴射器流れ
液体推薬ロケットエンジン
燃焼室
高圧
推薬燃焼
表面張力
ナビエ-ストークス方程式
numerical analysis
numerical simulation
injector flow
liquid propellant rocket engine
combustion chamber
high pressure
propellant combustion
surface tension
Navier-Stokes equation
Target Audience: 一般
Note (General): Numerical study on the jet flow in a high pressure fluid has been conducted in order to simulate atomization, mixing and combustion in a liquid rocket engine combustion chamber. The simulation results successfully show the break-up process of liquid oxygen jet in the high pressure hydrogen environment, while there is a little disagreement between the simulation results and theoretical estimations. Numerical results on the nitrogen jet flow agree well with the experimental results for the pressure higher than the critical point. It is suggested from the numerical results compared with experimental results that surface tension should be considered under the condition below the critical point.
資料番号: AA0049056001
レポート番号: JAXA-SP-05-010
Access Restrictions: 限定公開
Periodical Title (NCID): AA11984031
https://ci.nii.ac.jp/ncid/AA11984031
Data Provider (Database): 国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）
https://irdb.nii.ac.jp
Original Data Provider (Database): 宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ