Titlebook: Detonation Control for Propulsion; Pulse Detonation and Jiun-Ming Li,Chiang Juay Teo,Cheng Wang Book 2018 Springer International Publishing

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Review on the Research Progresses in Rotating Detonation Engine,ous Spin Detonation (CSD) and a few essential facts from the prior publications. Furthermore, a summarization of the Continuous Detonation Wave Rocket Engine (CDWRE) concepts is examined. At long last, a detailed numerical investigation and experiment work of RDE is also presented.

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Brennan Decker,Lynette M. Shollressure preheated air supply system was constructed which allows to supply air at rate of a few kg/s, preheated to more than 100 °C and at initial pressure up to 2.5 bar. Supply system for Jet-A fuel which could be preheated to 170 °C was also constructed. Additionally gaseous hydrogen supply system

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Jessica L. Dillon,Laura J. Tafeerformed to examine the impact of the DLRE configuration and fuel supply parameters on the operation process and thrust performance. In experiments, the absolute pressures of NG and oxygen supply were up to 30 and 15 atm, respectively; the mass flow rate of the reactive mixture was varied from 0.05

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Marie-Lisa Eich,George J. Nettoormed using the detailed chemistry model. The comparison of the MUSCL and the 5th-order RWCNS (WCNS5MN) indicates that the shock front and the contact surface for the WCNS5MN can be improved with the better resolution than those for the MUSCL and that both rotating velocities are approximately 97% o

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https://doi.org/10.1007/978-1-4939-7280-7ity was the first to conduct numerical and experimental research of the CDE in China. We designed several types of CDE combustion chambers and carried out experiments to verify its feasibility. In addition, we have performed a series of two- and three-dimensional simulations of the CDE. Numerical st

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