Thermal Effects on Cavitation Instabilities in Helical Inducers
Author:
Affiliation:
1. Alta S.p.A., 56121 Pisa, Italy
2. University of Pisa, 56100 Pisa, Italy
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/10.2514/1.12582
Reference18 articles.
1. Cavitation in Turbopumps—Part 1
2. Hydraulic and mechanical performance of LE-7 LOX pump inducer
3. Experimental Study on Rotating Cavitation of Rocket Propellant Pump Inducers
4. Observations of Oscillating Cavitation of an Inducer
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