Bolted double-lap composite joints under mechanical and thermal loading

International Journal of Solids and Structures

Volumn 38, Issue 44-45, 2001, Pages 7801-7837

  Kradinov, V ^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

Bolt; Composite; Double lap; Joint; Mechanical; Thermal

Indexed keywords

LAMINATED COMPOSITES; STIFFNESS; STRESS CONCENTRATION; STRESSES; THERMAL LOAD;

CONTACT STRESSES;

JOINTS (STRUCTURAL COMPONENTS);

JOINT;

EID: 0035850723     PISSN: 00207683     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0020-7683(01)00128-7     Document Type: Article

References (9)

1. Analysis of an infinite plate containing radial cracks originating at the boundary of an internal circular hole
2. On design methods for bolted joints in composite aircraft structures
3. Analysis of composite laminates with multiple fasteners
4. Analysis of composite laminates with multiple fasteners
5. Analysis of double-lap composite joints with multiple-row bolts under combined mechanical and thermal loading
6. A design model for composite joints with multiple fasteners