• Bài trích
  • Nhan đề: Constant single-buckle imperfection principle to determine a lower bound for the buckling load of unstiffened composite cylinders under axial compression /H.N.R. Wagner ⇑ , C. Hühne, S. Niemann

Tác giả CN Wagner,H.N.R.
Nhan đề Constant single-buckle imperfection principle to determine a lower bound for the buckling load of unstiffened composite cylinders under axial compression /H.N.R. Wagner ⇑ , C. Hühne, S. Niemann
Từ khóa tự do Buckling
Từ khóa tự do Cylindrical composite shells
Từ khóa tự do Single-perturbation load approach (SPLA)
Nguồn trích Composite structures2016-5 Số: 1 Tập: 139
00000000nab#a2200000ui#4500
00116100
0026
00436B44FBD-3965-4381-9FFD-61D5A0D6F4F1
005201708180750
008081223s vm| vie
0091 0
039|y20170818075644|zcuonglv
100 |aWagner,H.N.R.
245 |aConstant single-buckle imperfection principle to determine a lower bound for the buckling load of unstiffened composite cylinders under axial compression /H.N.R. Wagner ⇑ , C. Hühne, S. Niemann
653 |aBuckling
653 |aCylindrical composite shells
653 |aSingle-perturbation load approach (SPLA)
773 |tComposite structures|v139|i1|d2016-5
890|c1|a0|b0|d4
Không tìm thấy biểu ghi nào
Copyrights © Thư Viện Trường ĐH XÂY DỰNG HÀ NỘI