✦ LIBER ✦

Higher-Order Buckling of Debonded (Delaminated) Sandwich Panels with Soft Core

✍ Scribed by Frostig, Y.; Sokolinsky, V.

Book ID: 120467534
Publisher: American Institute of Aeronautics and Astronautics
Year: 2000
Tongue: English
Weight: 430 KB
Volume: 38
Category: Article
ISSN: 0001-1452
DOI: 10.2514/2.878

No coin nor oath required. For personal study only.

📜 SIMILAR VOLUMES

Similitude of sandwich panels with a ‘so

Similitude of sandwich panels with a ‘soft’ core in buckling

✍ Y. Frostig; G.J. Simitses 📂 Article 📅 2004 🏛 Elsevier Science 🌐 English ⚖ 219 KB

The paper presents the similarity analysis of a sandwich unidirectional panel with a transversely flexible core under buckling loads. The governing equations are those used in the high-order analysis of sandwich panels with a 'soft' core. The study derives the similitude conditions in the case of ex

Boundary Condition Effects in Buckling o

Boundary Condition Effects in Buckling of “Soft” Core Sandwich Panels

✍ Sokolinsky, V.; Frostig, Y. 📂 Article 📅 1999 🏛 American Society of Civil Engineers 🌐 English ⚖ 233 KB

Finite element buckling analysis of lami

Finite element buckling analysis of laminated composite sandwich panels with transversely flexible core containing a face/core debond

✍ Sayyidmousavi, A.; Malekzadeh, K.; Bougharara, H. 📂 Article 📅 2011 🏛 SAGE Publications 🌐 English ⚖ 378 KB

Improving delamination resistance capaci

Improving delamination resistance capacity of sandwich composite columns with initial face/core debond

✍ N. Mitra; B.R. Raja 📂 Article 📅 2012 🏛 Elsevier Science 🌐 English ⚖ 990 KB

Consistent Higher-Order Dynamic Equation

Consistent Higher-Order Dynamic Equations for Soft-Core Sandwich Beams

✍ Sokolinsky, Vladimir S.; Nutt, Steven R. 📂 Article 📅 2004 🏛 American Institute of Aeronautics and Astronautics 🌐 English ⚖ 433 KB

Thermal Buckling and Postbuckling of San

Thermal Buckling and Postbuckling of Sandwich Panels with a Transversely Flexible Core

✍ Frostig, Y.; Thomsen, O. T. 📂 Article 📅 2008 🏛 American Institute of Aeronautics and Astronautics 🌐 English ⚖ 916 KB