Traction Boundary Conditions in Hybrid-Stress Finite-Element Model-Reference-Cited by-同舟云学术

Traction Boundary Conditions in Hybrid-Stress Finite-Element Model

Published:1978-05 Issue:5 Volume:16 Page:529-531
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Atluri Satya N.¹,Rhee H. C.¹

Affiliation:

1. Georgia Institute of Technology, Atlanta, Ga.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.60920

Reference8 articles.

1. JAtIuri, S. N., Advances in Computer Methods for Partial Differentia! Equations, edited by Vichnevetsky, Rutgers University Press, New Brunswick, N. J., pp.346-356.

2. An assumed stress hybrid finite element method for an incompressible and near-incompressible material

3. 5Rhee, H. C. "On the Accuracy of Finite Element Solutions of Problems of Bending of Plates with Traction Boundary Conditions," Ph.D. Thesis, Georgia, lost,of Technology, 1977.

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