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The Influence of Sweep on Axial Flow Turbine Aerodynamics in the Endwall Region

Author
PULLAN, Graham1 ; HARVEY, Neil W2
[1] Whittle Laboratory, Department of Engineering, University of Cambridge, Cambridge CB3 ODY, United Kingdom
[2] Rolls-Royce plc, Derby DE24 8BJ, United Kingdom
Source

Journal of turbomachinery. 2008, Vol 130, Num 4 ; 041011.1-041011.10 ; ref : 15 ref

CODEN
JOTUEI
ISSN
0889-504X
Scientific domain
Mechanical engineering; Mechanics acoustics
Publisher
American Society of Mechanical Engineers, New York, NY
Publication country
United States
Document type
Article
Language
English
Keyword (fr)
Aile flèche Aube turbine Aérodynamique Ecoulement axial Ecoulement irrotationnel Ecoulement lent Ecoulement secondaire Etude expérimentale Moyeu Perte pression Structure turbulence Symétrie axiale Turbine axiale Turbine gaz Turbomachine
Keyword (en)
Swept wing Turbine blade Aerodynamics Axial flow Irrotational flow Slow flow Secondary flow Experimental study Hub Pressure loss Turbulence structure Axial symmetry Axial turbine Gas turbine Turbomachine
Keyword (es)
Ala flecha Paleta turbina Aerodinámica Flujo axial Flujo irrotacional Flujo lento Flujo secundario Estudio experimental Cubo Pérdida presión Estructura turbulencia Simetría axial Turbina axial Turbina gas Turbomáquina
Classification
Pascal
001 Exact sciences and technology / 001D Applied sciences / 001D12 Mechanical engineering. Machine design / 001D12F Engines and turbines / 001D12F02 Continuous cycle engines: steam and gas turbines, jet engines

Discipline
Mechanical engineering. Mechanical construction. Handling
Origin
Inist-CNRS
Database
PASCAL
INIST identifier
20707831

Sauf mention contraire ci-dessus, le contenu de cette notice bibliographique peut être utilisé dans le cadre d’une licence CC BY 4.0 Inist-CNRS / Unless otherwise stated above, the content of this bibliographic record may be used under a CC BY 4.0 licence by Inist-CNRS / A menos que se haya señalado antes, el contenido de este registro bibliográfico puede ser utilizado al amparo de una licencia CC BY 4.0 Inist-CNRS

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