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Heat transfer and effectiveness on film cooled turbine blade tip models

Author
KIM, Y. W.F; METZGER, D. E
Arizona State univ., dep. mechanical aerospace eng., Tempe AZ 85287, United States
Conference name
International gas turbine and aeroengine congress and exposition (38 ; Cincinnati OH 1993-05-24)
Source

Journal of turbomachinery. 1995, Vol 117, Num 1, pp 12-21 ; ref : 18 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
Conference Paper
Language
English
Keyword (fr)
Aube turbine Champ température Convection Ecoulement secondaire Etude expérimentale Refroidissement film Transfert chaleur Turbine axiale Turbine gaz Visualisation
Keyword (en)
Turbine blade Temperature distribution Convection Secondary flow Experimental study Film cooling Heat transfer Axial turbine Gas turbine Visualization
Keyword (es)
Paleta turbina Campo temperatura Convección Flujo secundario Estudio experimental Enfriamiento por película Transferencia térmica Turbina axial Turbina gas Visualización
Classification
Pascal
001 Exact sciences and technology / 001D Applied sciences / 001D06 Energy / 001D06D Energy. Thermal use of fuels / 001D06D03 Equipments for energy generation and conversion: thermal, electrical, mechanical energy, etc / 001D06D03D Engines and turbines

Discipline
Energy
Origin
Inist-CNRS
Database
PASCAL
INIST identifier
3490095

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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