1. Green PD. Current and future problems in structural acoustic fatigue. In: AGARD symposium, volume impact of acoustic loads on aircraft structures; 1994. p. 1.1–1.5.
2. European Aviation Safety Agency. Proof of structure – fatigue and damage tolerance. In: AMC 20–29 composite aircraft, structure; 2010.
3. ASTM-D6115. Standard test method for mode I fatigue delamination growth onset of unidirectional fiber-reinforced polymer matrix composite; 1997.
4. Development of a standardized procedure for the characterization of interlaminar delamination propagation in advanced composites under fatigue mode I loading conditions;Brunner;Eng Fracture Mech,2009
5. Mode II fatigue delamination resistance of advanced fiber-reinforced polymere matrix laminates: towards the development of a standardized test procedure;Brunner;Int J Fatigue,2012