Annular combustor for miniature jet engines

W. C. Ho, Y. C. Chao, D. B. Shiung

Research output: Contribution to journalArticlepeer-review

1 Citation (Scopus)

Abstract

A new miniature annular combustion system has been developed for a small existing turbojet engine. Simple V-gutter flameholding and radial fuel injection are employed to achieve flame stabilization. From airflow distribution tests, equivalence ratio in the primary-zone is varied in the range 0.63-0.72, yielding continuous combustion. Intensive combustion is generated by the presence of the V-gutter flameholders and fuel-air premixing. Size and length limitations provide a strong impact on distribution of fuel and dilution of hot gas.

Original languageEnglish
Pages (from-to)105-115
Number of pages11
JournalInternational Journal of Turbo and Jet Engines
Volume14
Issue number2
DOIs
Publication statusPublished - 1997

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering

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