[A-7] Liquid Rocket 3

[2022-a-27] Inducer Cavitation Control via Inlet Swirl

*Christopher Groll^1,2,Tobias Traudt², Michael Oschwaldt², Stefan Schlechtriem², Armin Herbertz³ ( 1. University of Stuttgart, Institute of Space Systems, Germany, 2. German Aerospace Center, Institute of Space Propulsion, Germany, 3. European Space Agency, ESTEC, Netherlands)

キーワード：Cavitation, Methane, Turbopump, Inducer, Swirl