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Thermo-Mechanical Modeling of a High Pressure Turbine Blade of an Airplane Gas Turbine Engine

AuthID
P-00M-7YZ

Author(s)

Brandao, P

Infante, V

Deus, AM

Editor(s)

Iacoviello,F;Reis,L;Fonte,M;Freitas,M;Infante,V

Document Type

Proceedings Paper

Year published

2016

Published

in XV PORTUGUESE CONFERENCE ON FRACTURE, PCF 2016 in Procedia Structural Integrity, ISSN: 2452-3216

Volume: 1, Pages: 189-196 (8)

Conference

15Th Portuguese Conference on Fracture (Pcf), Date: FEB 10-12, 2016, Location: Paco de Arcos, PORTUGAL, Sponsors: Instituto Super Tecnico, Sociedade Portuguesa Materiais, Fracture Div, European Struct Integr Soc

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Metadata
Sources

Publication Identifiers

DOI: 10.1016/j.prostr.2016.02.026

SCOPUS: 2-s2.0-85054342974

Wos: WOS:000387291100025

Source Identifiers

ISSN: 2452-3216

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Thermo-Mechanical Modeling of a High Pressure Turbine Blade of an Airplane Gas Turbine Engine

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