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A mechanism of combustion instability in lean premixed gas turbine combustors : Internal Combustion Engines

Author
LIEUWEN, T1 ; TORRES, H1 ; JOHNSON, C1 ; ZINN, B. T1
[1] Schools of Aerospace and Mechanical Engineering, Georgia Institute of Technology, Atlanta, GA 30332-0150, United States
Conference name
International Gas Turbine and Aeroengine Congress and Exhibition (Indianapolis, IN 1999-06-07)
Source

Journal of engineering for gas turbines and power. 2001, Vol 123, Num 1, pp 182-189 ; ref : 20 ref

CODEN
JETPEZ
ISSN
0742-4795
Scientific domain
Energy; Mechanical engineering
Publisher
American Society of Mechanical Engineers, New York, NY
Publication country
United States
Document type
Conference Paper
Language
English
Keyword (fr)
Chambre combustion Combustion Dégagement chaleur Gaz pauvre Injection combustible Instabilité Performance Prémélange Rapport air combustible Turbine gaz
Keyword (en)
Combustion chamber Combustion Heat liberation Lean gas Fuel injection Instability Performance Premixing Air fuel ratio Gas turbine
Keyword (es)
Cámara combustión Combustión Desprendimiento calor Gas pobre Inyección combustible Inestabilidad Rendimiento Premezcla Relación aire combustible Turbina gas
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
950349

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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