Corotational Nonlinear Dynamic Analysis of Thin-Shell Structures with Finite Rotations-Reference-Cited by-同舟云学术

Corotational Nonlinear Dynamic Analysis of Thin-Shell Structures with Finite Rotations

Published:2015-03 Issue:3 Volume:53 Page:663-677
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Yang Jinsong¹,Xia Pinqi¹

Affiliation:

1. Laboratory of Rotorcraft Aeromechanics, College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, 210016 Nanjing, People’s Republic of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J053147

Reference36 articles.

1. A unified formulation of small-strain corotational finite elements: I. Theory

2. Applications of higher order corotational stretch theories to nonlinear finite element analysis

3. An Element Independent Corotational Procedure for the Treatment of Large Rotations

4. Finite rotation analysis and consistent linearization using projectors

5. A unified co-rotational framework for solids, shells and beams

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