1. Haresceugh RI, Rogers GW, Shaw C, Woolstencroft DH. Development of an advanced technology wing. In: Middleton DH editor, Composite materials in aircraft structures. Longman Scientific & Technical; 1990. p. 249–59
2. Minguet PJA, O’Brien TK, Analysis of composite skin/stringer bond failure using a strain energy release rate approach. In: Proceedings of the 10th International Conference on Composite Materials, ICCM-10; 1995. p. I.245–52
3. Spier EE, On experimental versus theoretical incipient buckling of narrow graphite/epoxy plates in compression. In: AIAA Paper No. 80-0686. In: Proceedings of the AIAA/ASME/ASCE/AHS 21st Structures, Structural Dynamics and Materials Conference; 1980. p. 187–93
4. Bonanni DL, Johnson ER, Starnes Jr JH. Local crippling of thin-walled graphite-epoxy stiffeners. In: AIAA Paper No. 88-2251, Proceedings of the AIAA/ASME/ASCE/AHS 29th Structures, Structural Dynamics and Materials Conference, Part––1; 1988. p. 313–24
5. Scott ML, Cheung AKH, Newman PD. Design, analysis and testing of postbuckling co-cured composite control surface. In: ICAS-96-5.5.1, Proceedings of the 20th Congress of International Council of Aeronautical Sciences; 1996. p. 1137–47