Numerical simulation of shear dual-coaxial gas-gas injector

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Abstract

The turbulent Navier-Stokes equations in combination with two equation k-ε turbulence models were used to simulate the flow field of shear dual-coaxial single element GO2/GH2injector chamber. The results show that: the shear dual-coaxial injector has two shear combustion surfaces, enabling to achieve a high combustion efficiency at the condition of large mass flowrate, the oxygen injection velocity and the velocity ratio of hydrogen to oxygen are key parameters for shear dual-coaxial injector design, a lower oxygen injection velocity makes the combustion location far away from the faceplate, while a higher velocity ratio makes the combustion location closer to the faceplate. Compared with the gas-liquid shear coaxial injector, a faster oxygen injection velocity and proper velocity ratio of hydrogen to oxygen are preferable choice for design of shear dual-coaxial injector.

Original languageEnglish
Pages (from-to)829-834
Number of pages6
JournalHangkong Dongli Xuebao/Journal of Aerospace Power
Volume25
Issue number4
StatePublished - Apr 2010

Keywords

  • Gas-gas injector
  • Mass flowrate
  • Navier-Stokes equations
  • Numerical simulation

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