Rhys Jones
- Fractals and the lead crack airframe lifing framework. In: Procedia Structural Integrity, v. 2 ( 2016). (2016):
- Modified Hartman-Schijve fitting of mode I delamination fatigue data and the resulting variation in threshold values Gthr. In: Procedia Structural Integrity, v. 2 ( 2016). (2016):
- A means for industry to determine the economic life of bonded joints under representative operation flight loads. In: Procedia Structural Integrity, v. 28 ( 2020). (2020):
- A note on computing the growth of small cracks in AM Ti-6Al-4V. In: Procedia Structural Integrity, v. 28 ( 2020). (2020):
- A way forward for industry to determine valid cyclic-fatigue relationships for polymer-matrix fibre composites. In: Procedia Structural Integrity, v. 28 ( 2020). (2020):
- A unified constitutive theory for paper. In: Composite Structures, v. 42, n. 1 (Mai 1998). (1998):
- Development of life extension strategies for Australian military aircraft, using structural health monitoring of composite repairs and joints. In: Composite Structures, v. 66, n. 1-4 (Oktober 2004). (2004):
- Effect of corrosion and fatigue on the remaining life of structures and its implication to additive manufacturing. In: Frattura ed Integrità Strutturale, v. 12, n. 45 (Juli 2018). (2018):