Experimental Characterization of Cavitation Instabilities in the Avio "FAST2" Inducer
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American Institute of Aeronautics and Astronautics
Reference14 articles.
1. Hydraulic and mechanical performance of LE-7 LOX pump inducer
2. Observations of Oscillating Cavitation of an Inducer
3. 6Zoladz T. "Observations on Rotating Cavitation and Cavitation Surge from the Development of the Fastrac Engine Turbopump", 2000,36th AIAA/ASME/SAE/ASEE JointPropulsion Conference, Huntsville, AL, USA, July17-19.
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