Prediction of heat transfer characteristics for discrete hole film cooling - one row of injection into a turbulent boundary layer

Daneshmund K. Tafti, Savash Yavuzkurt

Research output: Contribution to journalArticlepeer-review

Original languageEnglish (US)
Pages (from-to)235-266
Number of pages32
JournalInternational Journal of Turbo and Jet Engines
Volume8
Issue number3-4
DOIs
StatePublished - 1991

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering

Cite this