JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
Online ISSN : 2432-3691
Print ISSN : 1344-6460
ISSN-L : 1344-6460
Articles
Effect of the Casing Configurations on the Internal Flow and Unsteady Pressure Fluctuation in Rocket Pump Inducer
Mitsuru ShimagakiHiroyuki HagaTomoyuki HashimotoMitsuo WatanabeSatoshi HasegawaTakashi ShimuraKenjiro Kamijo
Author information
JOURNAL FREE ACCESS

2005 Volume 53 Issue 617 Pages 266-273

Details
Abstract
The effects of the inlet casing configurations on unsteady cavitation were examined with a 3-bladed inducer. The inlet flow and cavitation pattern in two different casings were visualized using PIV (particle image velocimetry) and high-speed video. It was found that the rotating cavitation would be suppressed when the tip clearance at the inducer inlet was increased. The vortex cavitation in tip leakage flow and cavitation in back flow is considered to affect the appearance of the rotating cavitation by the inlet casing configuration.
Content from these authors
© 2005 The Japan Society for Aeronautical and Space Sciences
Previous article Next article
feedback
Top