Improvements in strength and stress corrosion cracking properties in aluminum alloy 7075 via low-temperature retrogression and re-aging heat treatments

Corrosion

Volumn 59, Issue 6, 2003, Pages 520-528

  Ferrer, C P ^a   Koul, M G ^a   Connolly, B J ^a   Moran, A L ^a  

^a UNITED STATES NAVAL ACADEMY   (United States)

Author keywords

AA7075; Aging aircraft; Re aging heat treatments; Retrogression; Stress corrosion cracking

Indexed keywords

AGING OF MATERIALS; AIRCRAFT; CANTILEVER BEAMS; HEAT TREATMENT; STRESS CORROSION CRACKING;

ALTERNATE IMMERSION;

ALUMINUM ALLOYS;

ALUMINUM ALLOY; CORROSION; STRENGTH ASSESSMENT; STRESS CORROSION CRACKING; TEMPERATURE EFFECT;

EID: 0038166950     PISSN: 00109312     EISSN: None     Source Type: Journal    
DOI: 10.5006/1.3277583     Document Type: Article

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