Reheat effect on the improvement in efficiency of the turbine driven by pulse detonation

Author:

Liu JunyuORCID,Wang Zhiwu,Zhang Zixu,Li Junlin,Qin Weifeng,Huang Jingjing

Funder

National Natural Science Foundation of China

Northwestern Polytechnical University

Natural Science Foundation of Shaanxi Province

Basic and Applied Basic Research Foundation of Guangdong Province

Publisher

Elsevier BV

Subject

Metals and Alloys,Mechanical Engineering,Ceramics and Composites,Computational Mechanics

Reference47 articles.

1. Progress of continuously rotating detonation engines;Zhou;Chin J Aeronaut,2016

2. Effects of total pressures and equivalence ratios on kerosene/air rotating detonation engines using a paralleling CE/SE method;Wang;Defence Technol,2021

3. Numerical simulation of flow field characteristics and the improvement of pressure oscillation of rotating detonation engine;Han;Defence Technol,2022

4. Pulse detonation propulsion: challenges, current status, and future perspective;Roy;Prog Energy Combust Sci,2004

5. Experimental study on the detonation process of a pulse detonation engine with ionized seeds;Lin;Defence Technol,2020

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