Application of unified fatigue damage approach to compression-tension region

International Journal of Fatigue

Volumn 21, Issue SUPPL. 1, 1999, Pages

  Vasudevan, A K ^a   Sadananda, K ^b  

^a OFFICE OF NAVAL RESEARCH   (United States)

^b NAVAL RESEARCH LABORATORY   (United States)

Author keywords

K; Aluminum alloys; Environment; Fatigue crack growth; Kmax; Load ratio; Mechanism; Microstructure; Nickel alloys; Steel; Titanium

Indexed keywords

ALUMINUM ALLOYS; CARBON STEEL; COMPRESSIVE STRESS; FATIGUE OF MATERIALS; LOADS (FORCES); NICKEL ALLOYS; TENSILE STRESS; TITANIUM;

COMPRESSION LOADS; COMPRESSION TENSION REGION; CYCLIC DAMAGE; LOAD RATIO; UNIFIED FATIGUE DAMAGE APPROACH;

CRACK PROPAGATION;

EID: 0033226935     PISSN: 01421123     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

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