Skip to main navigation Skip to search Skip to main content

Numerical simulation of leading edge film-cooling in a turbine cascade

Research output: Contribution to journalArticlepeer-review

Original languageEnglish
Pages (from-to)623
Number of pages1
JournalHangkong Dongli Xuebao/Journal of Aerospace Power
Volume18
Issue number5
StatePublished - Oct 2003

Cite this