Buckling of Laminated Composite Rectangular Plates-Reference-Cited by-同舟云学术

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Buckling of Laminated Composite Rectangular Plates

Published:2005-10 Issue:4 Volume:18 Page:215-223
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Shukla K. K.¹²³⁴,Nath Y.¹²³⁴,Kreuzer E.¹²³⁴,Kumar K. V.¹²³⁴

Affiliation:

1. Reader, Applied Mechanics Dept., M.N.N.I.T., Allahabad-04, India.

2. Professor, Applied Mechanics Dept., Indian Institute of Technology, Delhi-16, India.

3. Professor, TUHH, Meerestechnik II, Essendorfer Str. 42, 21073 Hamburg, Germany.

4. Graduate Student, Applied Mechanics Dept. Indian Institute of Technology, Delhi-16, India.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%290893-1321%282005%2918%3A4%28215%29

Reference19 articles.

1. Optimization of shear-deformable laminated plates under buckling and strength criteria

2. Dynamic instability of composite laminates using a higher order theory

3. Three-dimensional elasticity solution for buckling of composite laminates

4. Effect of Face-Sheet Anisotropy on Buckling and Postbuckling of Sandwich Plates

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