Rotating cavitation in three and four-bladed inducers-Reference-Cited by-同舟云学术

Rotating cavitation in three and four-bladed inducers

Published:1997-07-06 Issue: Volume: Page:
ISSN:
Container-title:33rd Joint Propulsion Conference and Exhibit
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Author:

Hashimoto Tomoyuki¹,Yamada Hitoshi¹,Funatsu Shiro²,Ishimoto Jun²,Kamijo Kenjiro²,Tsujimoto Yoshinobu³,Hashimoto Tomoyuki¹,Yamada Hitoshi¹,Funatsu Shiro²,Ishimoto Jun²,Kamijo Kenjiro²,Tsujimoto Yoshinobu³

Affiliation:

1. National Aerospace Lab., Kakuda, Japan

2. Tohoku Univ., Sendai, Japan

3. Osaka Univ., Toyonaka, Japan

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1997-3026

Reference7 articles.

1. Hydraulic and mechanical performance of LE-7 LOX pump inducer

2. Experimental Study on Rotating Cavitation of Rocket Propellant Pump Inducers

3. The Space Shuttle Main Engine liquid oxygen pump high-synchronous vibration issue, the problem, the resolution approach, the solution

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