Stress Intensity Factor Calculation in Cracked Aluminum PlatesRepaired with Various Composite Patch Configurations
محل انتشار: دومین کنفرانس بین المللی مهندسی مکانیک و هوافضا
سال انتشار: 1396
نوع سند: مقاله کنفرانسی
زبان: انگلیسی
مشاهده: 532
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شناسه ملی سند علمی:
MECHAERO02_402
تاریخ نمایه سازی: 13 شهریور 1396
چکیده مقاله:
Plates used as bearing structures in aircrafts usually suffer from defects as cracks. Therefore they should be either replaced or repaired somehow.In the present study, the effect of adhesively-bonded repair patch on stress intensity factor (SIF) is investigated for different crack types (semi-elliptical, through-thickness) located at the center of a rectangular aluminum plate. Results show that repaired plated have significantly lower SIF than unrepaired ones. Also it was seen that double-sided patches have much higher effect on SIF than singlesidedones. The structure is numerically modeled using ABAQUS and ZENCRACK followed by a finite element analysis to calculate J contour integrals and indeed SIF.
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نویسندگان
Seyed Mohammad Hossein Sharifi
Department of Mechanical Engineering, Petroleum University of Technology, Ahwaz, Iran
Hadi Eskandari
Abadan Institute of Technology, Petroleum University of Technology, Abadan, Iran
Arash Dehghani
Department of Mechanical Engineering, Petroleum University of Technology, Ahwaz, Iran