Evaluation of residual stress depth profiling in 7075 aluminum alloy plates

Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica

Volumn 24, Issue 4, 2003, Pages 336-338

  Wang, Qiu Cheng ^a   Ke, Ying Lin ^a   Zhang, Qiao Fang ^b  

^a ZHEJIANG UNIVERSITY   (China)

^b ZHEJIANG UNIVERSITY OF TECHNOLOGY   (China)

Author keywords

Aluminum alloy; Crack compliance method; Evaluation; Interior residual stress; Measurement; Stress gradient

Indexed keywords

AIRCRAFT MATERIALS; ALUMINUM ALLOYS; EVALUATION; MEASUREMENTS; RESIDUAL STRESSES;

CRACK COMPLIANCE METHOD; INTERIOR RESIDUAL STRESS; STRESS GRADIENT;

PLATES (STRUCTURAL COMPONENTS);

EID: 0842290789     PISSN: 10006893     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (5)

1. Wang Q C, Ke Y L. Control and relief of residual stresses in high-strength aluminum alloy parts for aerospace industry [J]. Journal of Aeronautical Materials, 2002, 22(3): 59-62.
2. Prime M B. Residual stress measurement by successive extension of a slot: the crack compliance method [J]. Applied Mechanics Reviews, 1999, 52(2): 75-96.
3. Prime M B, Hill M R. Residual stress, stress relief, and inhomogeneity in aluminum plate [J]. Scripta Materialia, 2002, 46 (1): 77-82
4. Lu J. Handbook of measurement of residual stresses [M]. Georgia, USA: The Fairmont Press, 1996. 5-21,108-109
5. Chakrabarti D J, Weiland H, Cheney B A, etc. Through-thickness property variations in 7050 plate [J]. Materials Science Forum, 1996, 217-222: 1085-1090.