Skip to main navigation Skip to search Skip to main content

Investigation of rotating detonation fueled by the pre-combustion cracked kerosene

  • Yepan Zhong
  • , Yun Wu
  • , Di Jin
  • , Xin Chen
  • , Xingkui Yang
  • , Shunli Wang
  • Air Force Engineering University Xian

Research output: Contribution to journalArticlepeer-review

96 Scopus citations

Abstract

In this study, a method of pre-combustion cracking is adopted in the investigation of the rotating detonation fueled by kerosene. The basic characteristics of the rotating detonation wave (RDW) including the wave speed, pressure, and propagating modes are researched. The wave speed increases when the equivalence ratio is near the stoichiometric ratio, but it is little affected by the flow rates. Different to the wave speed performance, the pressure of the RDW tends to increase when the flow rates rise but show weak relation with the ER. Features and transition of the five rotating detonation modes including the two-co rotating waves, two-counter rotating waves, single-wave, pop-out and failure mode are investigated. The lean fuel boundary of the RDW is broadened with the increase of the flow rates. Also, the effect of the oxygen ratio (50% and 30%) of the oxidizer (oxygen-enriched air) on the characteristics of the RDW is investigated. The rotating detonation using oxidizer with the higher oxygen ratio has a better speed performance than with the lower oxygen ratio.

Original languageEnglish
Article number105480
JournalAerospace Science and Technology
Volume95
DOIs
StatePublished - Dec 2019

Keywords

  • Mode transition
  • Oxygen ratio
  • Pre-combustion cracked kerosene
  • Rotating detonation

Fingerprint

Dive into the research topics of 'Investigation of rotating detonation fueled by the pre-combustion cracked kerosene'. Together they form a unique fingerprint.

Cite this