A Reduced Order Model for Preliminary Design and Performance Prediction of Tapered Inducers: Comparison with Numerical Simulations
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Publisher
American Institute of Aeronautics and Astronautics
Reference18 articles.
1. 2Ashihara, K., Goto, A., Kamijo, K., Yamada, H., Uchiumi, M., 2002, "Improvements of Inducer Inlet Backflow Characteristics Using 3-D Inverse Design Method", 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Indianapolis, USA.
2. Cavitation in Turbopumps—Part 1
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