Thermal stresses in aluminum-to-composite double-lap bonded joints

Advances in Engineering Software

Volumn 29, Issue 3-6, 1998, Pages 273-281

  Rastogi, Naveen ^a   Soni, Som R ^a   Nagar, Arvind ^b  

^a AdTech Systems Research Inc   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ALUMINUM; COMPOSITE STRUCTURES; EPOXY RESINS; FINITE ELEMENT METHOD; GLASS FIBER REINFORCED PLASTICS; GRAPHITE FIBER REINFORCED PLASTICS; PLASTIC LAMINATES; STRESS ANALYSIS; STRUCTURAL ANALYSIS; THERMAL EXPANSION; THERMAL STRESS; VARIATIONAL TECHNIQUES;

DOUBLE LAP BONDED JOINTS;

ADHESIVE JOINTS;

EID: 0032041180     PISSN: 09659978     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0965-9978(97)00079-3     Document Type: Article

References (4)

1. Baker, A. A. and Jones, R. (Eds), Bonded Repair of Aircraft Structures. Martinus Nijhoff Publishers, Boston, 1988.
2. Fredell, R. S., Damage tolerant repair techniques for pressurized aircraft fuselages, Rep. No. WL-TR-94-3137, Flight Dynamics Directorate, Wright-Patterson Air Force Base, Dayton, OH 45433, June, 1994.
3. Rastogi, N., Variable-order elements for three-dimensional linear elastic structural analysis - I: mathematical formulations. Computers and Structures, 1997 (submitted for publication).
4. Rastogi, N., Variable-order elements for three-dimensional linear elastic structural analysis - II: illustrative examples. Computers and Structures, 1997 (submitted for publication).