Application of thermal boundary layer integral method on a jet vane system

M. S. Yu, H. H. Cho, K. Y. Hwang, J. C. Bae

Research output: Chapter in Book/Report/Conference proceedingConference contribution


The boundary layer integral method is used for the thermal analysis of a jet vane system. The integral boundary layer equations are suggested to be applied for several distinguishable flow regions around a vane surface. The changes of temperature distribution in a jet vane are explained with the flow phenomena around it and the quantitative values show a good agreement with the experimental result.

Original languageEnglish
Title of host publication38th AIAA Thermophysics Conference
Publication statusPublished - 2005
Event38th AIAA Thermophysics Conference - Toronto, ON, Canada
Duration: 2005 Jun 62005 Jun 9

Publication series

Name38th AIAA Thermophysics Conference


Other38th AIAA Thermophysics Conference
CityToronto, ON

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Mechanical Engineering
  • Condensed Matter Physics


Dive into the research topics of 'Application of thermal boundary layer integral method on a jet vane system'. Together they form a unique fingerprint.

Cite this