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 contributionResearchpeer-review

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

Cite this

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. / Marn, Andreas; Göttlich, Emil; Malzacher, Franz; Pirker, Hermann-Peter.

ASME Turbo Expo. ., 2009. p. 1-15.

Research output: Chapter in Book/Report/Conference proceedingConference contributionResearchpeer-review

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AU - Malzacher, Franz

AU - Pirker, Hermann-Peter

PY - 2009

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M3 - Conference contribution

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BT - ASME Turbo Expo

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