Bolted patch repair of composite panels with a cutout

Composite Structures

Volumn 56, Issue 4, 2002, Pages 423-444

  Kradinov, V ^a   Hanauska, J ^a   Barut, A ^a   Madenci, E ^a   Ambur, D R ^b  

^a University of Arizona   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

Composites; Cutout; Multiple bolts; Patch; Repair

Indexed keywords

SIGNAL FILTERING AND PREDICTION; STRUCTURAL PANELS;

COMPOSITE PANELS;

COMPOSITE STRUCTURES;

AIRCRAFT; COMPOSITE; LOADING; REPAIR;

EID: 0036624211     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0263-8223(02)00027-2     Document Type: Article

References (9)

1. Fatigue issues in aircraft maintenance and repair
2. Finite element design and analysis of a bolted patch repair for composites
3. The failure analysis of bolted repair on composite laminate
4. Analysis of fastened structural connections
5. Bolted field repair of graphite/epoxy wing skin laminates
6. Analysis of single- and double- Lap composite joints with multiple-row bolts under combined mechanical and thermal loading
7. Analysis of an infinite plate containing radial cracks originating at the boundary of an internal circular hole