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Autor:
Md. Fuad Shah Koslan, Ahmad Zaidi Ahmad Mujahid, Gunasilan Manar, Shohaimi Abdullah, Mohd Salleh Bin Mohd Tahir
Publikováno v:
Applied Mechanics and Materials. 471:267-272
The majority of aircrafts structure cracks due to fatigue are thin gage metallic structures and secondary support structures. Beside lower fatigue strength, they may also occur due to mechanical defects, especially at weak area and for areas exposed