A comparison of honeycomb-core and foam-core carbon-fibre/epoxy sandwich panels

Composites - Tập 21 Số 4 - Trang 325-331 - 1990
M. Akay1, R.E.B. Hanna2
1Department of Mechanical and Industrial Engineering, University of Ulster at Jordanstown, Newtownabbey, Co. Antrim, BT37 0QB, Northern Ireland
2Research and Development into aircraft components with Short Brothers plc, Airport Road, Belfast, Northern Ireland

Tóm tắt

Từ khóa


Tài liệu tham khảo

Jones, 1985, Compressive failures of damaged graphite epoxy laminates, Composite Struct., 3, 167, 10.1016/0263-8223(85)90042-X

Bishop, 1985, The mechanical performance and impact behaviour of carbon-fibre reinforced PEEK, Composite Struct., 3, 295, 10.1016/0263-8223(85)90059-5

Rhodes, 1979, Low velocity impact damage in graphite-fiber reinforced epoxy laminates

Dorey, 1975, Fracture behaviour and residual strength of carbon fibre composites subjected to impact loads

Akay, 1988, Relaxation transitions, fracture toughness and post-impact residual capacity of carbon-fibre reinforced composites, Composites Sci. Technol., 33, 1, 10.1016/0266-3538(88)90052-8

Oplinger, 1975, Impact damage tolerance of graphite/epoxy sandwich panels, Foreign Object Impact Damage to Composites ASTM STP, 568, 30, 10.1520/STP33149S

Rhodes, 1978, Impact tests on fibrous composite sandwich structures, NASA TM 78719

Sharma, 1981, Low-velocity impact tests on fibrous composite sandwich structures, Test Methods and Design Allowables for Fibrous Composites ASTM STP, 734, 54, 10.1520/STP29303S

Bernard, 1987, Impact resistance of composite sandwich panels, 167

't Hart, 1981

Akay, 1989, Influence of curing conditions and post-cure hygrothermal treatment on the mechanical behaviour of carbon fibre/epoxy laminates, 155