𝔖 Bobbio Scriptorium

✦ LIBER ✦

Finite Element Computation of Woven Ply Laminated Composite Structures up to Rupture

✍ Scribed by Cyril Bordreuil; Christian Hochard

Book ID: 111569840
Publisher: Springer Netherlands
Year: 2004
Tongue: English
Weight: 423 KB
Volume: 11
Category: Article
ISSN: 0929-189X
DOI: 10.1023/b:acma.0000026474.67067.b6

No coin nor oath required. For personal study only.

📜 SIMILAR VOLUMES

Behaviour up to rupture of woven ply lam

Behaviour up to rupture of woven ply laminate structures under static loading conditions

✍ Ch. Hochard; S. Miot; N. Lahellec; F. Mazerolle; M. Herman; J.P. Charles 📂 Article 📅 2009 🏛 Elsevier Science 🌐 English ⚖ 606 KB

Nonstationary random response of laminat

Nonstationary random response of laminated composite structures by a hybrid strain-based laminated flat triangular shell finite element

✍ C.W.S. To; B. Wang 📂 Article 📅 1996 🏛 Elsevier Science 🌐 English ⚖ 567 KB

The finite element analysis of composite

The finite element analysis of composite laminates and shell structures subjected to low velocity impact

✍ Shiuh-Chuan Her; Yu-Cheng Liang 📂 Article 📅 2004 🏛 Elsevier Science 🌐 English ⚖ 984 KB

Cross-ply laminates with holes in compre

Cross-ply laminates with holes in compression: straight free-edge stresses determined by two- to three-dimensional global/local finite element analysis: Thompson, D.M., Griffin, O.H. and Vidussoni, M.A. Journal of Composites Technology and Research Vol 12 No 4 (1990) pp 209–216

📂 Article 📅 1991 🏛 Elsevier Science ⚖ 154 KB

[American Institute of Aeronautics and A

[American Institute of Aeronautics and Astronautics 45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference - Palm Springs, California ()] 45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference - Coupled Finite Element for Non-linear Laminated Piezoelectric Composite Shells with Applications to Buckling and Postbuckling Behavior

✍ Varelis, Dimitris; Saravanos, Dimitris 📂 Article 📅 2004 🏛 American Institute of Aeronautics and Astronautics ⚖ 161 KB