ロケットエンジンの燃料ミキサー特性に及ぼすミキサー形状の影響について

Material type: 文書・図像類

Author: 小野寺, 卓郎ほか

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)：: Effects of liquid hydrogen mixer configurations on its downstream flow field were investigated. Cryogenic tests with different mixer configurations of...

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Material Type: 文書・図像類
Title: ロケットエンジンの燃料ミキサー特性に及ぼすミキサー形状の影響について
Author/Editor: 小野寺, 卓郎
坂本, 博
高橋, 守
佐々木, 正樹
田村, 洋
木村, 俊哉
谷口, 浩文
Onodera, Takuo
Sakamoto, Hiroshi
Takahashi, Mamoru
Sasaki, Masaki
Tamura, Hiroshi
Kimura, Toshiya
Taniguchi, Hirofumi
Author Heading: 小野寺, 卓郎
坂本, 博
高橋, 守
佐々木, 正樹
田村, 洋
木村, 俊哉
谷口, 浩文
Onodera, Takuo
Sakamoto, Hiroshi
Takahashi, Mamoru
Sasaki, Masaki
Tamura, Hiroshi
Kimura, Toshiya
Taniguchi, Hirofumi
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: Effects of configurations of a mixer in a rocket engine upon its downstream flow field
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: 41-42
ISSN (Periodical Title): ISSN : 1349-113X
Text Language Code: jpn
Subject Heading: ロケットエンジン設計
燃料ミキサー
液体燃料ロケットエンジン
液体水素
超臨界流れ
多相流
圧力変動
CFD
rocket engine design
fuel mixer
liquid propellant rocket engine
liquid hydrogen
supercritical flow
multiphase flow
pressure fluctuation
Target Audience: 一般
Note (General): Effects of liquid hydrogen mixer configurations on its downstream flow field were investigated. Cryogenic tests with different mixer configurations of eight patterns and CFD analysis were conducted. It was found that mixer configurations have strong effects on low-frequency pressure fluctuation levels at downstream positions and that these pressure fluctuations are strongly related to acoustic oscillations in the hydrogen tube end of the mixer.
資料番号: AA0049056008
レポート番号: JAXA-SP-05-010
Source: https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=6239&item_no=1&attribute_id=31&file_no=1
https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=6239&item_no=1&attribute_id=31&file_no=1
Access Restrictions: 限定公開
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