CRACK-CLOSURE MODEL FOR PREDICTING FATIGUE CRACK GROWTH UNDER AIRCRAFT SPECTRUM LOADING.

ASTM Special Technical Publication

Volumn , Issue 748, 1981, Pages 53-84

  Newman Jr , J C ^a  

^a NONE

Author keywords

[No Author keywords available]

Indexed keywords

ALUMINUM AND ALLOYS - FATIGUE; FAILURE ANALYSIS - MATHEMATICAL MODELS; MATERIALS TESTING - PLASTICITY; STESSES - SPECTRUM ANALYSIS;

AIRCRAFT MATERIALS;

EID: 0019627111     PISSN: 10403094     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (20)