2018•Acta AstronauticaRequires access

Numerical and experimental investigation on the influence of inlet contraction ratio for a rocket-based combined cycle engine

Zhang Zhengze, Peijin Liu, Fei Qin, Lei Shi, Yajun Wang, Chao Huo

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Key concepts: Inlet, Mechanics, Discharge coefficient, Overall pressure ratio, Thrust, Materials science, Combustor, Rocket engine

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Numerical and experimental investigation on the influence of inlet contraction ratio for a rocket-based combined cycle engine — Research Paper | ScholarLens