Nine-Node Resultant-Stress Shell Element for Free Vibration and Large Deflection of Composite Laminates-Reference-Cited by-同舟云学术

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Nine-Node Resultant-Stress Shell Element for Free Vibration and Large Deflection of Composite Laminates

Published:2006-04 Issue:2 Volume:19 Page:103-120
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Han S. C.¹²³,Choi S.¹²³,Chang S. Y.¹²³

Affiliation:

1. Associate Professor, Dept. of Civil Engineering, Daewon Science College, Jecheon, Chungbuk, 390-702 Korea (corresponding author).

2. Structural Engineer, Division of Structural Engineering, EO Engineers Co. Ltd., Anyang 431-060, Korea.

3. Professor, Dept. of Civil Engineering, Univ. of Seoul, Seoul 130-732, Korea.

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%282006%2919%3A2%28103%29

Reference38 articles.

1. Analysis of thick and thin shell structures by curved finite elements

2. Assumed strain stabilization procedure for the 9-node Lagrange shell element

3. Development of a one point quadrature shell element for nonlinear applications with contact and anisotropy

4. An automatic arc length algorithm for tracing equilibrium paths of nonlinear structures;Chaisomphob T.;Proc., JSCE,1988

5. A fast incremental/iterative solution procedure that handles “snap-through”

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