Experimental study of repair efficiency for single-sided composite patches bonded to aircraft structural panels

• SATO Masaki

  Department of Aeronautics and Space Engineering, Tohoku University

• YOKOBORI A. Toshimitsu JR.

  Fracture Research Institute, Tohoku University

• OZAWA Yoshihito

  Faculty of Education, Fukushima University

• KAMIYAMA Takayuki

  Aerospace Division, Fuji Heavy Industries Ltd.

• MIYANAGA Toshiaki

  Nippon Steel Chemical Co., Ltd.

• BEAUMONT P. W. R.

  Department of Engineering, University of Cambridge

• SEKINE Hideki

  Department of Aeronautics and Space Engineering, Tohoku University

Journal

• Advanced composite materials : the official journal of the Japan Society for Composite Materials

  Advanced composite materials : the official journal of the Japan Society for Composite Materials 11 (1), 51-59, 2002-03-01

Keywords

• Patch repair
• composite patch
• crached aluminum panel
• repair efficiency
• stress intensity range
• environmental condition

Details

• CRID: 1570572699716141568
• NII Article ID: 10008580749
• NII Book ID: AA10744021
• ISSN: 09243046
• Text Lang: en
• Data Source:
  • CiNii Articles