Failure analysis of stress corrosion cracking in aircraft bolts

Engineering Failure Analysis

Volumn 14, Issue 1, 2007, Pages 209-217

  Lee, Hong Chul ^a   Choi, Jae man ^a   Lee, Bokwon ^a   Kim, Tae Gu ^b  

^a Aerospace Technology Research Institute   (South Korea)

^b Inje University   (South Korea)

Author keywords

Clamp bolt; Residual stress; Stress corrosion cracking

Indexed keywords

BOLTS; FAILURE (MECHANICAL); FRACTOGRAPHY; RESIDUAL STRESSES; STRESS ANALYSIS; STRESS CORROSION CRACKING;

AIRCRAFT BOLTS; CLAMP BOLT; CORROSIVE ENVIRONMENT; SUSCEPTIBLE ALLOYS;

CLAMPING DEVICES;

BOLTS; CLAMPING DEVICES; FAILURE (MECHANICAL); FRACTOGRAPHY; RESIDUAL STRESSES; STRESS ANALYSIS; STRESS CORROSION CRACKING;

EID: 33746761688     PISSN: 13506307     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.engfailanal.2005.10.021     Document Type: Article

References (6)

1. Smith W.F. Structure and properties of engineering alloys (1993), McGraw-Hill p. 303-312
2. Juvinall R.C., and Marshek K.M. Fundamentals of machine component design (1991), Wiley p. 365
3. Jones R.H. Stress-corrosion cracking; materials performance and evaluation (1999), ASM p. 121
4. ASM metals handbook vol. 13 (1992), ASM International p. 489
5. TCTO 1F-4-1616. Inspection of V-band coupling; 1997.
6. Davis J.R. Corrosion: understanding the basics (2003), ASM p. 256