Effects of pitting corrosion on the fatigue behavior of aluminum alloy 7075-T6: Modeling and experimental studies

Materials Science and Engineering: A

Volumn 297, Issue 1-2, 2001, Pages 223-229

  Sankaran, K K ^a   Perez, R ^a   Jata, K V ^b  

^a BOEING COMPANY   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

Accelerated corrosion tests; Corrosion fatigue; Corrosion metrics; Fatigue life prediction; Pitting corrosion

Indexed keywords

ALUMINUM ALLOY; FATIGUE LIFE ANALYSIS; PITTING CORROSION; SIZE DISTRIBUTION;

AIRCRAFT MATERIALS; CRACK INITIATION; FATIGUE TESTING; MATHEMATICAL MODELS; PITTING;

ALUMINUM ALLOY 7075 T6; CORROSION FATIGUE;

ALUMINUM ALLOYS;

EID: 0035105216     PISSN: 09215093     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0921-5093(00)01216-8     Document Type: Article

References (11)

1. Model for prediction of fatigue lives based upon a pitting corrosion fatigue process
2. Effects of prior corrosion on the S/N fatigue performance of aluminum alloys 2024-T3 and 2524-T3
3. Materials evaluation using wet-dry mixed salt spray tests