Modelling the sources of cracking of aircraft compressor vanes rings

Engineering Failure Analysis

Volumn 12, Issue 5 SPEC. ISS., 2005, Pages 699-710

  Nash, D H ^a   Dempster, I R ^b  

^a UNIVERSITY OF STRATHCLYDE   (United Kingdom)

^b Wyman Gordon Forgings   (United States)

Author keywords

Cracking; Damage; Stress analysis; Thermal analysis; Turboprop

Indexed keywords

AIRCRAFT ENGINES; COMPRESSORS; CRACK INITIATION; FINITE ELEMENT METHOD; LOADING; MATHEMATICAL MODELS; STRESS ANALYSIS;

AIRCRAFT COMPRESSOR VANES RINGS; CRACK ASSESSMENT; FINITE ELEMENT MODELS; HIGH SERVICE LIFE DUTY;

RINGS (COMPONENTS);

COMPRESSOR; CRACKING;

EID: 21844454454     PISSN: 13506307     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.engfailanal.2004.12.017     Document Type: Article

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