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Numerical modeling and simulation of turbine test rig combustion device (I) partition model based on mixture fraction

  • Beihang University
  • Beijing Aerospace Measurement and Control Corp.

Research output: Contribution to journalArticlepeer-review

Abstract

A system-level modularization numerical model which can deal with the coupling effect of combustion and flow was established for combustion device, with air and kerosene as reactants, of a turbine test rig and its outlet section, and a thermodynamic calculation scheme based on mixture fraction and a mixture fraction equation were put forward. Comparison with simulation results of the model based on mass-flow-rate mixture ratio and experimental results indicates that the mixture fraction-based model can solve the problem of transient simulation stability in the previous research, and reach the accuracy of simulation consistent with experimental results.

Original languageEnglish
Pages (from-to)981-986
Number of pages6
JournalTuijin Jishu/Journal of Propulsion Technology
Volume33
Issue number6
StatePublished - Dec 2012

Keywords

  • Combustion device
  • Liquid propellant rocket engine
  • Mixture fraction
  • Numerical simulation
  • Turbine test rig

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