Experimental Investigation of Detonation Propagation Modes and Thrust Performance in a Small Rotating Detonation Engine Using C<sub>2</sub>H<sub>4</sub>/O<sub>2</sub> Propellant

Experimental Investigation of Detonation Propagation Modes and Thrust Performance in a Small Rotating Detonation Engine Using C<sub>2</sub>H<sub>4</sub>/O<sub>2</sub> Propellant

A small rotating detonation engine (RDE) model and the corresponding experimental setup were constructed for the experimental investigation of the detonation propagation characteristics and thrust performance of a circular RDE. Experiments were conducted at a range of 0.3–2.5 equivalence ratio with...

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Bibliographic Details
Main Authors: Hyung-Seok Han, Eun Sung Lee, Jeong-Yeol Choi
Format: Article
Language:English
Published: MDPI AG 2021-03-01
Series:Energies
Subjects:
pressure gain combustion
rotating detonation engine
detonation propagation characteristics
thrust performance
Online Access:https://www.mdpi.com/1996-1073/14/5/1381

Internet

https://www.mdpi.com/1996-1073/14/5/1381

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