Now showing items 1-6 of 6

    • Buckling analysis of thick-walled composite pipe under external pressure 

      Yang, Chihdar Charles; Pang, Su-Seng; Zhao, Yi (SAGE Publications, 1997-02)
      Composite pipe has been used in transporting corrosive fluid in many chemical processes in the petrochemical and pulp and paper industries. It is often subjected to external pressures due to process conditions (vacuum), ...
    • Elastic-plastic analysis of adhesive-bonded single-lap composite joints under tension 

      Yang, Chihdar Charles; Pang, Su-Seng (American Society of Mechanical Engineers(ASME), 1993-07)
      An analytical model of adhesive-bonded single-lap composite joints is developed to predict the stress-strain distributions with such joints under tensile loading. The First-order laminated anisotropic plate theorem is ...
    • Fracture analysis of adhesive-bonded single-lap composite joints 

      Sun, Wenjun; Yang, Chihdar Charles (Society for the Advancement of Material and Process Engineering, 2004-05)
      A fracture mechanics model to estimate the energy release rate of adhesive-bonded single-lap composite joints under tension has been developed. The stress distributions of the adhesive-bonded single-lap composite joint ...
    • Strain energy release rate analysis of adhesive-bonded composite joints with a prescribed interlaminar crack 

      Chadegani, Alireza; Yang, Chihdar Charles; Dan-Jumbo, Eugene (American Institute of Aeronautics and Astronautics, 2009-01)
      Delamination is among the critical failure modes in fiber-reinforced laminated composite structures. This paper presents an analytical approach by taking into account the first-ply failure in adhesive-bonded composite ...
    • Stress-strain analysis of single-lap composite joints under tension 

      Yang, Chihdar Charles; Pang, Su-Seng (American Society of Mechanical Engineers (ASME), 1996-01)
      Based on the laminated anisotropic plate theory, an analytical model is proposed to determine the stress and strain distributions of adhesive-bonded composite single-lap joints under tension. The laminated anisotropic plate ...
    • Thermally induced loads of fastened hybrid composite/aluminum structures 

      Yang, Chihdar Charles; Sun, Wenjun; Seneviratne, Waruna P.; Shashidhar, Ananthram K. (American Institute of Aeronautics and Astronautics, 2008-03)
      Large composite structures have been increasingly used in the aviation industry. New applications of composite materials include primary structures such as aircraft fuselages. These large composite parts are sometimes ...