Fluid mechanics of pulse detonation thrusters |
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| Institution: | 1. College of Computer Science and Technology, National Huaqiao University, Xiamen 361021, China;2. Department of Electronic Engineering, Tsinghua University, Beijing 100084, China |
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| Abstract: | The advantages of constant volume combustion cycle as compared to constant pressure combustion in terms of thermodynamic efficiency have focused the researches of advanced propulsion on detonation engines. The paper gives coverage of efforts undertaken during past decades in adjusting detonations for propulsion applications, and highlights new challenges in studying fluid flow dynamics relevant to onset of detonation. |
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