The Influence of Rotor Tip Clearance Size on the Flow Through an S-Shaped Intermediate Turbine Duct Shortened by an Applying an Integrated Concept

Andreas Marn; Emil Göttlich; Thomas Leitgeb; Franz Heitmeir

The Influence of Rotor Tip Clearance Size on the Flow Through an S-Shaped Intermediate Turbine Duct Shortened by an Applying an Integrated Concept

Andreas Marn, Emil Göttlich, Thomas Leitgeb, Franz Heitmeir

Institut für Thermische Turbomaschinen und Maschinendynamik (3190)

Publikation: Konferenzbeitrag › (Altdaten) Vortrag oder Präsentation

Originalsprache	englisch
Publikationsstatus	Veröffentlicht - 23 März 2009
Veranstaltung	8th European Turbomachinery Conference: ETC08 - Graz, Österreich Dauer: 23 März 2009 → 27 März 2009

Sonstiges

Sonstiges	8th European Turbomachinery Conference
Land/Gebiet	Österreich
Ort	Graz
Zeitraum	23/03/09 → 27/03/09

Fields of Expertise

Mobility & Production

Treatment code (Nähere Zuordnung)

Experimental

EU - AIDA - Aggressive Intermediate Duct Aerodynamics for Competitve and Enviromentally Friendly Jet Engines
Pirker, H., Marn, A., Heitmeir, F., Woisetschläger, J., Sanz, W. & Göttlich, E.
1/02/04 → 31/01/08
Projekt: Forschungsprojekt

Dieses zitieren

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title = "The Influence of Rotor Tip Clearance Size on the Flow Through an S-Shaped Intermediate Turbine Duct Shortened by an Applying an Integrated Concept",

author = "Andreas Marn and Emil G{\"o}ttlich and Thomas Leitgeb and Franz Heitmeir",

year = "2009",

month = mar,

day = "23",

language = "English",

note = "8th European Turbomachinery Conference : ETC08 ; Conference date: 23-03-2009 Through 27-03-2009",

}

TY - CONF

T1 - The Influence of Rotor Tip Clearance Size on the Flow Through an S-Shaped Intermediate Turbine Duct Shortened by an Applying an Integrated Concept

AU - Marn, Andreas

AU - Göttlich, Emil

AU - Leitgeb, Thomas

AU - Heitmeir, Franz

PY - 2009/3/23

Y1 - 2009/3/23

M3 - (Old data) Lecture or Presentation

T2 - 8th European Turbomachinery Conference

Y2 - 23 March 2009 through 27 March 2009

ER -

The Influence of Rotor Tip Clearance Size on the Flow Through an S-Shaped Intermediate Turbine Duct Shortened by an Applying an Integrated Concept

Sonstiges

Fields of Expertise

Treatment code (Nähere Zuordnung)

Projekte

EU - AIDA - Aggressive Intermediate Duct Aerodynamics for Competitve and Enviromentally Friendly Jet Engines

Dieses zitieren