Relation Between Geometries of Inducer Inlet and Backflow and Vortex Structures
Author:
Affiliation:
1. Japan Aerospace Exploration Agency
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2004-4022
Reference8 articles.
1. 2Ryan,R.S.,Gross,L.A.,Mills,D.,andMichell,P."TheSpaceShuttleMainEngineLiquidOxygenPumpHigh-Synchronous Vibration Issue, theProblem, theResolution Approach, theSolution," AIAAPaper 94-3153,1994.
2. Observations of Oscillating Cavitation of an Inducer
3. Hydraulic and mechanical performance of LE-7 LOX pump inducer
4. 5Hashimoto, T., Komatsu, T., Kamijo, K., Hasegawa, S., Watanabe, M., and Yamada, H. "Observation of Backflow and Prewhirl at Rocket PropellantPump Inducer,"AIAAPaper 2000-3154, July2000.
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3. Numerical Simulation Research on Vortex Characteristics of Centrifugal Pump Inlet Recirculation;Advanced Materials Research;2012-02
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