Volume 27 Issue 4
Apr.  2012
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Article Navigation >  Journal of Aerospace Power  > 2012  >  27(4): 861-867
TAN Wen-long, FAN Wei-jun, ZHANG Tao, WANG Wei-jian, ZHANG Rong-chun. Performance test of micro turbojet engine’s evaporator and numerical simulation of the combustor[J]. Journal of Aerospace Power, 2012, 27(4): 861-867.
Citation: TAN Wen-long, FAN Wei-jun, ZHANG Tao, WANG Wei-jian, ZHANG Rong-chun. Performance test of micro turbojet engine’s evaporator and numerical simulation of the combustor[J]. Journal of Aerospace Power, 2012, 27(4): 861-867.
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Performance test of micro turbojet engine’s evaporator and numerical simulation of the combustor

  • National Key Laboratory of Science and Technology on Aero-Engines Aero-thermodynamics, School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

  • Received Date: 2011-05-23
  • Rev Recd Date: 2011-09-16
  • Publish Date: 2012-04-28
    Abstract
  • An annular combustor supplied by evaporator for a micro turbojet engine which was used for 40daN level missile was designed.The evaporator’s atomization and evaporation rate data was obtaind by test and then used for the numerical simulation of the combustor.The CFD(computational fluid dynamics) simulation shows the structure of the combustor is reasonable and the performance meets the design point’s requirements.

     

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