References
- Hirose , Y. , Taki , T. , Mizusaki , Y. and Fujita , T. 2004 . Low cost structural concept for composite trailing edge flap . Adv. Composite Mater. , 12 : 281 – 300 .
- Hirose , Y. , Nishitani , M. , Imuta , M. , Fukagawa , H. and Kikukawa , H. 2003 . Development of foam core sandwich panel structure for transport nose component SME Technical Paper TP03PUB317
- Bruman , M. 1997 . Fatigue crack initiation and propagation in sandwich structures , Stockholm , , Sweden : Department of Aeronautics, Royal Institute of Technology . Report No. 98-29
- Shipsha , A. 2001 . Failure of sandwich structures with sub-interface damage , Stockholm , , Sweden : Department of Aeronautics, Royal Institute of Technology . Report 2001–13
- Herbeck , L. , Wilmes , H. and Kleineberg , M. 2004 . Material and processing technology for CFRPfuselage USA SAMPE
- JIS K 7086 Testing methods for interlaminar fracture toughness of carbon fiber reinforced plastics
- Hojo , M. , Kageyama , K. and Tanaka , Y. 1995 . Prestandardization study on mode I interlaminar fracture toughness test for CFRP in Japan . Composites , 26 : 243
- Tanaka , Y. , Kageyama , K. and Hojo , M. 1995 . Prestandardization study on mode II interlaminar fracture toughness test for CFRP In Japan . Composites , 26 : 57
- Russell , A. J. and Street , K. N. 1985 . “ Moisture and temperature effects on the mixed-mode delamination fracture of unidirectional graphite/epoxy ” . In ASTM STP876 , Edited by: Johnson , W. S. 349 – 370 . Philadelphia : American Society for Testing and Materials .
- Murri , G. B. , Salpekar , S. A. and O'Brien , T. K. 1991 . “ Fatigue delamination onset prediction in unidirectional tapered laminates ” . In Composite Materials: Fatigue and Fracture, ASTM STP1110 , Edited by: O'Brien , T. K. Vol. 3 , 312 – 339 . Philadelphia : American Society for Testing and Materials .
- Rybicki , E. F. and Kanninen , M. F. 1977 . A finite element calculation of stress intensity factors by a modified crack closure integral . Engng. Fract. Mech. , 9 : 931 – 938 .