Cavitation Performance and Instability of a Two-Bladed Inducer
Author:
Affiliation:
1. Hyundai Rotem Company, Uiwang 437-718, Republic of Korea
2. Seoul National University, Seoul 151-742, Republic of Korea
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.B34459
Reference13 articles.
1. Hydraulic and mechanical performance of LE-7 LOX pump inducer
2. Experimental Characterization of Cavitation Instabilities in a Two-Bladed Axial Inducer
3. Effects of Shaft Vibration on Occurrence of Asymmetric Cavitation in Inducer
4. Higher Order Rotating Cavitation in an Inducer
5. Effect of the Casing Configurations on the Internal Flow in Rocket Pump Inducer
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