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A numerical study of high pressure turbine forced response in the presence of damaged nozzle guide vanes

Author
DI MARE, L1 ; IMREGUN, M1 ; SMITH, A. D2 ; ELLIOTT, R2
[1] Vibration UTC Mechanical Engineering Department Imperial College London, London, United Kingdom
[2] Rolls-Royce Turbines -Design Engineering, Derby, United Kingdom
Source

Aeronautical Journal. 2007, Vol 111, Num 1125, pp 751-757, 7 p ; ref : 16 ref

CODEN
AENJAK
ISSN
0001-9240
Scientific domain
Aeronautics astronautics; Mechanics acoustics
Publisher
Royal Aeronautical Society, London
Publication country
United Kingdom
Document type
Article
Language
English
Keyword (fr)
Aube directrice Aérodynamique Aéroélasticité Endommagement Haute pression Modélisation Simulation numérique Turbine gaz Turboréacteur
Keyword (en)
Guide vane Aerodynamics Aeroelasticity Damaging High pressure Modeling Numerical simulation Gas turbine Turbojet
Keyword (es)
Paleta directora Aerodinámica Aeroelasticidad Deterioración Alta presión Modelización Simulación numérica Turbina gas Turboreactor
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
19885792

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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