Fatigue damage analysis of wing-fuselage attachment lug

Procedia Structural Integrity - Tập 5 - Trang 801-808 - 2017
Slobodanka Boljanović1, Stevan Maksimović2
1Mathematical Institute of the Serbian Academy of Sciences and Arts, Kneza Mihaila 36, Belgrade, 11000, Serbia
2VTI - Aeronautical Department, Ratka Resanovića 1, Belgrade 11000, Serbia

Tài liệu tham khảo

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