Thrust characteristics research on continuous rotating detonation engine
Detonation combustion can produce pressure enhancement effect, increasing engine thrust. In this paper, a 2D Euler control equation with chemical reaction is used to solve the periodic flow of the detonation wave in a rectangular plane. The combustion of the air-breathing continuous rotating detonat...
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Published in | Case studies in thermal engineering Vol. 47; p. 103127 |
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Main Authors | , |
Format | Journal Article |
Language | English |
Published |
Elsevier Ltd
01.07.2023
Elsevier |
Subjects | |
Online Access | Get full text |
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