John Wang
- Static and fatigue testing bolted, bonded and hybrid step lap joints of thick carbon fibre/epoxy laminates used on aircraft structures. In: Composite Structures, v. 142 (May 2016). (2016):
- Predicting matrix failure in composite structures using a hybrid failure criterion. In: Composite Structures, v. 137 (March 2016). (2016):
- Matrix failure in composite laminates under tensile loading. In: Composite Structures, v. 135 (January 2016). (2016):
- Static and fatigue testing thin riveted, bonded and hybrid carbon fiber double lap joints used in aircraft structures. In: Composite Structures, v. 121 (March 2015). (2015):