The Influence of Blade Tip Gap Variation On The Flow Through an Aggressive S-Shaped Intermediate Turbine Duct Downstream a Transonic Turbine Stage-Part I: Time Averaged Results.

Research output: Contribution to conference(Old data) Lecture or Presentation

Original languageGerman
Publication statusPublished - 13 Sept 2007
EventInterne Weiterbildung-MTU Aero Engines -
Duration: 13 Sept 200713 Sept 2007


ConferenceInterne Weiterbildung-MTU Aero Engines

Fields of Expertise

  • Mobility & Production

Treatment code (Nähere Zuordnung)

  • Experimental

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