The Effect of Rotor Tip Clearance Size onto the Separated Flow through a Super-Aggressive S-Shaped Intermediate Turbine Duct Downstream of a Transonic Turbine Stage

Research output: Contribution to journalArticlepeer-review

Original languageEnglish
Pages (from-to)051019-1-051019-12
JournalJournal of Turbomachinery
Publication statusPublished - 2012

Fields of Expertise

  • Mobility & Production

Treatment code (Nähere Zuordnung)

  • Experimental

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