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

Andreas Marn; Emil Göttlich; Franz Malzacher; Hermann-Peter Pirker

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

Andreas Marn, Emil Göttlich, Franz Malzacher, Hermann-Peter Pirker

Institut für Thermische Turbomaschinen und Maschinendynamik (3190)

Publikation: Beitrag in Buch/Bericht/Konferenzband › Beitrag in einem Konferenzband › Begutachtung

Originalsprache	englisch
Titel	ASME Turbo Expo
Herausgeber (Verlag)	.
Seiten	1-15
Publikationsstatus	Veröffentlicht - 2009
Veranstaltung	ASME Turbo Expo 2009: Turbomachinery Technical Conference & Exhibition - Orlando, USA / Vereinigte Staaten Dauer: 8 Juni 2009 → 12 Juni 2009

Konferenz

Konferenz	ASME Turbo Expo 2009
Land/Gebiet	USA / Vereinigte Staaten
Ort	Orlando
Zeitraum	8/06/09 → 12/06/09

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 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",

author = "Andreas Marn and Emil G{\"o}ttlich and Franz Malzacher and Hermann-Peter Pirker",

year = "2009",

language = "English",

pages = "1--15",

booktitle = "ASME Turbo Expo",

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note = "ASME Turbo Expo 2009 : Turbomachinery Technical Conference & Exhibition ; Conference date: 08-06-2009 Through 12-06-2009",

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TY - GEN

T1 - 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

AU - Marn, Andreas

AU - Göttlich, Emil

AU - Malzacher, Franz

AU - Pirker, Hermann-Peter

PY - 2009

Y1 - 2009

M3 - Conference paper

SP - 1

EP - 15

BT - ASME Turbo Expo

PB - .

T2 - ASME Turbo Expo 2009

Y2 - 8 June 2009 through 12 June 2009

ER -

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

Konferenz

Fields of Expertise

Treatment code (Nähere Zuordnung)

Projekte

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

Dieses zitieren