Experimental investigation of kerosene supersonic combustion test using aerated-liquid injectors

  • Liao Wang*
  • , Cheng Liang Zhang
  • , Bao Xi Wei
  • , Xu Xu
  • *Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

Abstract

Experimental investigation of kerosene supersonic combustion was performed on direct-connect supersonic combustion test facility by using aerated-liquid injectors. In the test, kerosene equivalence ratio was 0.97 and 0.33, and hydrogen, air and nitrogen were used as effervescent gas respectively. The experimental results show that, cavity flameholders can achieve kerosene self-ignition and flame-holding effect by producing an eddy with low speed and high temperature, kerosene can prolong the resident time in combustor and achieve sufficient heating by the effect of this eddy. The hydrogen can self-ignite and release energy while injecting into the supersonic combustor, therefore adding hydrogen by aerated-liquid injector can improve the combustion performance of kerosene, and even achieve stable combustion without cavity flameholder.

Original languageEnglish
Pages (from-to)353-359
Number of pages7
JournalHangkong Dongli Xuebao/Journal of Aerospace Power
Volume24
Issue number2
StatePublished - Feb 2009

Keywords

  • Aerated-liquid injector
  • Cavity flameholder
  • Scramjet
  • Supersonic combustion

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