33th Congress of the International Council of the Aeronautical Sciences

04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance

FATIGUE DAMAGE MODEL OF HIGH TEMPERATURE POLYMER COMPOSITES IN AERO-ENGINES

V.R. Pakkam Gabrielš, P. Fernbergš; šLuleå University of Technology, Sweden

Results from development of a methodology for prediction of consequences of the damage accumulation occurring during fatigue loading of fiber reinforced polymer composites (FRPC) are presented. The methodology is developed with the intention of being applied to temperature resistant FRPC with potential use in e.g. aeroengine applications.


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