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2015•CEAS Space JournalRequires access

Modeling and simulation of a GOX/kerosene subscale rocket combustion chamber with film cooling

C. Höglauer, Björn Kniesner, O. Knab, Gregor Schlieben, Christoph Kirchberger, Simona Silvestri, Oskar Haidn

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Key concepts: Combustion chamber, Propellant, Combustion, Aerospace engineering, Liquid-propellant rocket, Rocket (weapon), Kerosene, Heat transfer

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