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Method to calculate thermal load of a CCL body

  • Qiang Qi*
  • , Shi Hua Bi
  • , Wei Dong He
  • *Corresponding author for this work
  • Beijing Institute of Technology
  • China Space Science and Industry Group Co.

Research output: Contribution to journalArticlepeer-review

Abstract

By measuring point temperature on outer surface of a canister launcher, the corresponding point temperature on inner surface, average heat flux through cylinder wall, the possible highest temperature on outer surface were calculated out. With a group point temperatures along cylinder wall, a polynomial fitness method was applied to deduce the distribution function of heat flux along cylinder wall, and general heat absorption quantity and absorbed heat energy were estimated out of a canister body by integrating the distribution function. This method can be used in engineering designs practically.

Original languageEnglish
Pages (from-to)125-128
Number of pages4
JournalBinggong Xuebao/Acta Armamentarii
Volume27
Issue numberSUPPL.
Publication statusPublished - Mar 2006

Keywords

  • Jet flow heat transfer
  • Point temperature measurement
  • Polynomial fitness
  • Thermal load distribution
  • Thermology

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