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Numerical investigation of low cycle fatigue life for channel wall nozzles

  • Shanghai Institute of Space Propulsion
  • Shanghai Engineering Research Center of Space Engine

Research output: Contribution to journalArticlepeer-review

Abstract

The thermal-structural response and low cycle fatigue life of a three-dimensional (3D) channel wall nozzle with regenerative cooling were numerically investigated by coupling the finite volume fluid-thermal method, nonlinear finite element thermal-structural analysis and local strain methods. The nozzle had a high area ratio (nozzle exit area divided by throat area) under cyclic working loads. Parametric studies were carried out to evaluate the effects of channel structural parameters such as channel width, channel height, liner thickness and rib width. Results showed that the integrated effects of three-dimensional channel structure and load distribution caused serious strain, which mainly occurred at the intersectant regions of liner wall on the gas side and the symmetric planes of channel and rib. The cooling effect and channel structural strength were significantly improved as the channel width and height decreased, leading to substantial extension of the nozzle service life. On the other hand, the successive decrease in liner thickness and rib width apparently increased the strain amplitude and residual strain of channel wall nozzle during cyclic work, significantly shortening the service life. The present work is of value for design of the channel wall nozzle to prolong its cyclic service life.

Original languageEnglish
Pages (from-to)1553-1565
Number of pages13
JournalHangkong Dongli Xuebao/Journal of Aerospace Power
Volume33
Issue number7
DOIs
StatePublished - 1 Jul 2018

Keywords

  • Channel wall nozzle
  • Finite element method
  • Liquid propellant rocket engine
  • Low cycle fatigue
  • Nonlinear structural analysis
  • Regenerative cooling

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