PSDがターボポンプ上流配管の共鳴キャビテーションサージに与える影響

Material type: 文書・図像類

Author: 吉田, 義樹ほか

Publisher: 宇宙航空研究開発機構(JAXA)

Publication date: 2013-10-31

Material Format: Digital

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Note (General)：: To investigate the effect of PSD on acoustic cavitation surge in turbopump, we conducted analyses with the resistance of PSD as a parameter. Consequen...

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Material Type: 文書・図像類
Title: PSDがターボポンプ上流配管の共鳴キャビテーションサージに与える影響
Author/Editor: 吉田, 義樹
藤原, 徹也
南里, 秀明
Yoshida, Yoshiki
Fujiwara, Tetsuya
Nanri, Hideaki
Author Heading: 吉田, 義樹
藤原, 徹也
南里, 秀明
Yoshida, Yoshiki
Fujiwara, Tetsuya
Nanri, Hideaki
Publication, Distribution, etc.: 宇宙航空研究開発機構(JAXA)
Publication Date: 2013-10-31
Publication Date (W3CDTF): 2013-10-31
Alternative Title: Effect of PSD on Acoustic Cavitation Surge in Inlet Pipe of Turbopump
Periodical title: 宇宙航空研究開発機構研究開発資料 = JAXA Research and Development Memorandum
No. or year of volume/issue: JAXA-RM-13-002
Volume: JAXA-RM-13-002
Pages: 1-11
ISSN (Periodical Title): ISSN : 1349-1121
Text Language Code: jpn
Subject Heading: Acoustic Cavitation Surge
Resonance
PSD
Turbopump
Target Audience: 一般
Note (General): To investigate the effect of PSD on acoustic cavitation surge in turbopump, we conducted analyses with the resistance of PSD as a parameter. Consequently, we found that patterns of the acoustic cavitation surge were classified into three types by the value of the resistance. (1) First (the resistance of the PSD is smaller.), when the frequency of the inertial cavitation surge between the PSD and the turbopump coincides with the acoustic natural frequencies between the tank and the PSD, the acoustic cavitation surge onsets between the tank and the PSD. (2) Second (the resistance of the PSD is middle.), the inertial cavitation surge which occurs between the PSD and the turbopump is suppressed by the resistance of the PSD. However, when the frequency of the inertial cavitation surge between the PSD and the turbopump coincides with the acoustic natural frequencies between the tank and the turbopump, the acoustic cavitation surge onsets between the tank and the turbopump. (3) Third (the resistance of the PSD is larger.), when the effect of the PSD is lost, the acoustic cavitation surge just occurs between the tank and the turbopump with several harmonic frequencies.
形態: カラー図版あり
Physical characteristics: Original contains color illustrations
資料番号: AA0062011000
レポート番号: JAXA-RM-13-002
Access Restrictions: 限定公開
Periodical Title (NCID): AA11983593
https://ci.nii.ac.jp/ncid/AA11983593
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