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Numerical simulation on improved integrated afterburner scheme

  • Wei Long Wang
  • , Jie Jin
  • , Wen Ming Jing
  • , Deng Huan Liu
  • , He Ming Ji
  • , Qing Jiang You
  • , Jiang Ning Li

Research output: Contribution to journalArticlepeer-review

Abstract

An improved integrated afterburner scheme was proposed to solve the problem of too large mass of traditional afterburner and too significant flow loss in non-augmentation condition. This scheme canceled the conventional stabilizer of blunt body, and a sudden expanding structure of central cone for stabilizing the flame was adopted. Numerical simulation was conducted to research its performance. The result indicates that the scheme is not sensitive to inlet parameters; total pressure recovery coefficients of three schemes on all cases are greater than 0.96; afterburner efficiency is close to 0.90; the scheme with lobed mixer has the best overall performance.

Original languageEnglish
Pages (from-to)1119-1124
Number of pages6
JournalHangkong Dongli Xuebao/Journal of Aerospace Power
Volume30
Issue number5
DOIs
StatePublished - 1 May 2015

Keywords

  • Afterburner
  • Combustion efficiency
  • Integrated
  • Lobed mixer
  • Overall performance

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