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

Abstract

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 Dec 1
Event38th AIAA Thermophysics Conference - Toronto, ON, Canada
Duration: 2005 Jun 62005 Jun 9

Publication series

Name38th AIAA Thermophysics Conference

Other

Other38th AIAA Thermophysics Conference
CountryCanada
CityToronto, ON
Period05/6/605/6/9

    Fingerprint

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Mechanical Engineering
  • Condensed Matter Physics

Cite this

Yu, M. S., Cho, H. H., Hwang, K. Y., & Bae, J. C. (2005). Application of thermal boundary layer integral method on a jet vane system. In 38th AIAA Thermophysics Conference (38th AIAA Thermophysics Conference).