Wall heat transfer measurements in high-pressure combustion devices

  • Xiaowei Wang
  • , Yushan Gao
  • , Guobiao Cai*
  • , Hongfa Huo
  • *Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

Abstract

To investigate the wall heat transfer characteristics in a combustion chamber over a broad range of pressure conditions, a method of taking a series of wall temperature measurements in a heat sink combustion chamber, and calculating the wall temperature and heat flux from the temperature data, was introduced. The temperature and heat flux at the inner wall of the combustion chamber can be obtained using this method. The key parameters of the test article are presented, and the technique requirements for thermocouples are described. A two-dimensional (2D) axisymmetric numerical calculation method was developed to obtain the wall temperature and heat flux from the measured temperatures. The method was applied to a firing test of a single-element gaseous hydrogen/gaseous oxygen shear-coaxial injector chamber to demonstrate the details of the method. Furthermore, the heat transfer characteristics of a single-element combustion chamber at chamber pressures of 0.92 MPa to 6.1 MPa were investigated using this method. The results indicate that the wall heat flux of this gas-gas injector combustor has, qualitatively, the same distribution at different pressures and correlates quantitatively with the chamber pressure as q̇∼pc0.8.

Original languageEnglish
Pages (from-to)698-707
Number of pages10
JournalJournal of Aerospace Engineering
Volume26
Issue number4
DOIs
StatePublished - Oct 2013

Keywords

  • Heat flux
  • Heat transfer
  • Injector
  • Measurement
  • Temperature

Fingerprint

Dive into the research topics of 'Wall heat transfer measurements in high-pressure combustion devices'. Together they form a unique fingerprint.

Cite this