Sayar, B. And KAYRAN, A. 2014. Two-stage fatigue life evaluation of an aircraft fuselage panel with a bulging circumferential crack and a broken stringer. FATIGUE & FRACTURE OF ENGINEERING MATERIALS & STRUCTURES , vol.37, no.5 , 494-507.

Sayar, B., & KAYRAN, A., (2014). Two-stage fatigue life evaluation of an aircraft fuselage panel with a bulging circumferential crack and a broken stringer. FATIGUE & FRACTURE OF ENGINEERING MATERIALS & STRUCTURES , vol.37, no.5, 494-507.

Sayar, B., And ALTAN KAYRAN. "Two-stage fatigue life evaluation of an aircraft fuselage panel with a bulging circumferential crack and a broken stringer," FATIGUE & FRACTURE OF ENGINEERING MATERIALS & STRUCTURES , vol.37, no.5, 494-507, 2014

Sayar, B. And KAYRAN, ALTAN. "Two-stage fatigue life evaluation of an aircraft fuselage panel with a bulging circumferential crack and a broken stringer." FATIGUE & FRACTURE OF ENGINEERING MATERIALS & STRUCTURES , vol.37, no.5, pp.494-507, 2014

Sayar, B. And KAYRAN, A. (2014) . "Two-stage fatigue life evaluation of an aircraft fuselage panel with a bulging circumferential crack and a broken stringer." FATIGUE & FRACTURE OF ENGINEERING MATERIALS & STRUCTURES , vol.37, no.5, pp.494-507.

@article{article, author={B. Sayar And author={ALTAN KAYRAN}, title={Two-stage fatigue life evaluation of an aircraft fuselage panel with a bulging circumferential crack and a broken stringer}, journal={FATIGUE & FRACTURE OF ENGINEERING MATERIALS & STRUCTURES}, year=2014, pages={494-507} }