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

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

Original languageEnglish
Title of host publicationASME Turbo Expo
Publisher.
Pages1-15
Publication statusPublished - 2009
EventASME Turbo Expo 2009 - Orlando, Fla., United States
Duration: 8 Jun 200912 Jun 2009

Conference

ConferenceASME Turbo Expo 2009
CountryUnited States
CityOrlando, Fla.
Period8/06/0912/06/09

Fields of Expertise

  • Mobility & Production

Treatment code (Nähere Zuordnung)

  • Experimental

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