Accuracy of modal stress calculations by the finite element method

Author:

ADELMAN HOWARD M.1,CATHERINES DONNELL S.1,WALTON WILLIAM C.1

Affiliation:

1. NASA- Langley Research Center, Langley Station, Hampton, Va.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference13 articles.

1. Procedure

2. As regards number and placement of elements to represent the shell, five trials were made. First, the shell was represented by 10 equal elements as shown in Fig. 5a. Maintaining this layout of elements, calculations were made of the six quantities of interest in connection with the stresses using each of the polynomial expansions (1), (2), and (3) in the elements. The results of these calculations are compared with the exact theory in Figs. 6-11. There was no mixing of expansions among the elements; that is, when expansion (1) was used in any one element it was used in all elements and similarly for expansions (2) and (3). The representation

3. ANALYSIS OF AXISYMMETRICAL SHELLS BY THE DIRECT STIFFNESS METHOD

4. Application of matrix displacement method to linear elastic analysisof shells of revolution.

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