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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Grasiella A. Andriani,Cristina Montagnadetonation research facilities in Temasek Laboratories. The main objective is to understand the re-initiation mechanisms through shock reflections, and investigate the performance of detonation re-initiation at different test conditions. Stable and unstable detonation waves are both taken into consi

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978-3-319-88679-4Springer International Publishing AG 2018

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Detonation Control for Propulsion978-3-319-68906-7Series ISSN 2197-9529 Series E-ISSN 2197-9537

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Performance of Rotating Detonation Engines for Air Breathing Applications,Laboratory’s Detonation Engine Research Facility. The performance scaling characteristics observed between various physical device configurations is discussed; included is the influence of mass flow rate, air injection area ratio and nozzle area ratio. The impact of geometry on the unsteady nature o

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Development of Gasturbine with Detonation Chamber,ressure 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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Flow Structure in Rotating Detonation Engine with Separate Supply of Fuel and Oxidizer: Experiment erformed 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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