Notice of Retraction: Optimization design of the rocket launching facilities and the thermal protection

Yi Jiang*, Yan Li Ma, Wei Chen Wang, Ji Guang Hao

*Corresponding author for this work

Research output: Chapter in Book/Report/Conference proceedingChapterpeer-review

Abstract

Based on fully hexahedral mesh and the k-e turbulence model, the computational fluid dynamics method was used to the numerical simulation. Different angle of the double-faced deflector and the thermal protection of the launching facilities were calculated. The pressure and temperature parameters were obtained and the result was compared and analyzed. The appropriate model was selected. The numerical calculation method and the results can be used to the engineering.

Original languageEnglish
Title of host publicationProceedings - 2nd IEEE International Conference on Advanced Computer Control, ICACC 2010
PublisherIEEE Computer Society
Pages30-33
Number of pages4
ISBN (Print)9781424458462
DOIs
Publication statusPublished - 2010

Publication series

NameProceedings - 2nd IEEE International Conference on Advanced Computer Control, ICACC 2010
Volume5

Keywords

  • Deflector
  • Launching facilities
  • Rocket plume
  • Simulation
  • Thermal protection

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