Composite patch reinforcement of cracked aircraft upper longeron: analysis and specimen simulation

This publication has 11 references indexed in Scilit:

• Integrity of edge-debonded patch on cracked panel
  Theoretical and Applied Fracture Mechanics, 1989
• Isoparametric shear spring element applied to crack patching and instability
  Theoretical and Applied Fracture Mechanics, 1989
• Full scale fatigue crack growth test of advanced jet trainer AT-3
  Theoretical and Applied Fracture Mechanics, 1989
• Fibre composite repair of cracked metallic aircraft components — practical and basic aspects
  Composites, 1987
• Failure initiation in unnotched specimens subjected to monotonic and cyclic loading
  Theoretical and Applied Fracture Mechanics, 1984
• Repair of cracked or defective metallic aircraft components with advanced fibre composites—an overview of Australian work
  Composite Structures, 1984
• Crack growth resistance characterized by the strain energy density function
  Engineering Fracture Mechanics, 1983
• Fracture initiation under gross yielding: Strain energy density criterion
  Engineering Fracture Mechanics, 1983
• Neutral axis offset effects due to crack patching
  Composite Structures, 1983
• The collapsed cubic isoparametric element as a ingular element for crack probblems
  International Journal for Numerical Methods in Engineering, 1978