Hygrothermal analysis of composite wing T-joints

Aircraft Engineering and Aerospace Technology

Volumn 74, Issue 1, 2002, Pages 23-37

  Kumari, Shyama ^a   Sinha, P K ^a  

^a INDIAN INSTITUTE OF TECHNOLOGY   (India)

Author keywords

Composite materials; Finite element method; Joints; Stress

Indexed keywords

BOUNDARY CONDITIONS; CARBON FIBERS; DEGRADATION; FINITE ELEMENT METHOD; LAMINATED COMPOSITES; MOISTURE; RESIDUAL STRESSES; SERVICE LIFE; STIFFNESS; THERMAL EFFECTS;

CARBON FIBER COMPOSITES (CFC); HYGROTHERMAL ANALYSIS;

JOINTS (STRUCTURAL COMPONENTS);

EID: 0036248270     PISSN: 00022667     EISSN: None     Source Type: Journal    
DOI: 10.1108/00022660210415001     Document Type: Article

References (15)

1. A higher-order theory of hygrothermal behaviour of laminated composite shells
2. Hygrothermal stresses and strains in axisymmetric composite shells
3. On the hygrothermal response of laminated composite systems
4. Effects of shear deformation and anisotropy on the thermal bending of layered composite plates
5. Exact solution of moderately thick laminated shells
6. Failure analysis of composite T-joints including inserts
7. Hygrothermal effects on the bending characteristics of laminated composite plates
8. Thermal stress analysis of laminated composite plates and shells
9. Thermoelastic analysis of laminated plates. 1: Symmetric specially orthotropic laminates
10. Thermoelastic analysis of laminated plates. 2: Anti-symmetric cross-ply and angle-ply laminates
11. Effects of environment on the elastic response of layered composite plates