Increasing the fatigue life of cracked fastener holes using bonded repairs
Tóm tắt
Từ khóa
Tài liệu tham khảo
Baker, 1978, A summary of work on applications of advanced fibre composites at the Aeronautical Research Labs, J. Composites, 9, 11, 10.1016/0010-4361(78)90512-8
Jones, 1984, Bonded repair of damage, J. Aero. Soc. India, 36, 193
Baker, 1984, Repair of Mirage III aircraft using BFRP crack patching technique, Theoret. Appl. Fracture Mech., 2, 1, 10.1016/0167-8442(84)90035-1
Jones, 1982, Crack patching analysis and design, J. Struct. Mech., 10, 177, 10.1080/03601218208907409
Gran, 1971, Investigation and analysis development of early life aircraft structural failures
Jones, 1981, New thoughts on stopping cracks which emanate from holes, Int. J. Fracture, 17, R53, 10.1007/BF00036197
Mann, 1984, The use of adhesively bonded rivets to reduce the effects of rivet holes on fatigue life, ARL Structures Report, 399
Heller, 1986, Analysis of bonded inserts for the repair of fastener holes, J. Engng. Fracture Mech., 24, 523, 10.1016/0013-7944(86)90226-2
Broek, 1977