Composite repairs to cracks in thick metallic components

Composite Structures

Volumn 44, Issue 1, 1999, Pages 17-29

  Jones, R ^a   Chiu, W K ^a  

^a MONASH UNIVERSITY   (Australia)

Author keywords

[No Author keywords available]

Indexed keywords

SURFACE FLAWS;

CRACKS; STRUCTURAL ANALYSIS; SURFACES;

COMPOSITE STRUCTURES;

EID: 0032686270     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0263-8223(98)00108-1     Document Type: Article

References (17)

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3. [3] Baker AA, Callinan RJ, Davis MJ, Jones R, Williams JG. Repair of Mirage iii aircraft using BFRP crack patching technology, Theoretical and Applied Fracture Mechanics (1984);2:1-16.
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13. [13] ASTM D 1002, Standard test method for strength properties of adhesives in shear by tension loading (Metal to Metal), ASTM Standards Vol. 15.06 Sec. 15 ASTM, Philadelphia, 1990:45.
14. [14] Damage Tolerance and Fatigue Evaluation of Structure, Federal Aviation Administration Advisory Circular, 25.571-1A, 1986.
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