Failure analysis of a second stage blade in a gas turbine engine

Engineering Failure Analysis

Volumn 15, Issue 8, 2008, Pages 1111-1129

  Poursaeidi, E ^a,b   Aieneravaie, M ^b   Mohammadi, M R ^b  

^a UNIVERSITY OF ZANJAN   (Iran)

^b Iran Power Plant Repairs Co   (Iran)

Author keywords

Blade failure; Fatigue failure; Finite element; Hot corrosion; Inconel 738LC

Indexed keywords

CORROSION FATIGUE; CRACK INITIATION; FAILURE ANALYSIS; FINITE ELEMENT METHOD; FRACTOGRAPHY; HARDNESS; HARMONIC ANALYSIS; NICKEL ALLOYS; STRESSES; TURBOMACHINE BLADES;

CAMPBELL DIAGRAM; HARDNESS MEASUREMENT; HOT CORROSION; STATIC STRESSES;

GAS TURBINES;

CORROSION FATIGUE; CRACK INITIATION; FAILURE ANALYSIS; FINITE ELEMENT METHOD; FRACTOGRAPHY; GAS TURBINES; HARDNESS; HARMONIC ANALYSIS; NICKEL ALLOYS; STRESSES; TURBOMACHINE BLADES;

EID: 41949112987     PISSN: 13506307     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.engfailanal.2007.11.020     Document Type: Article

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