Buckling of rectangular sandwich plates subjected to edgewise compression with loaded edges simply supported and unloaded edges clamped / Kuo Tai Yen, V.L. Salerno, and N.J. Hoff.
Saved in:
| Main Author: | |
|---|---|
| Corporate Author: | |
| Other Authors: | , |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1952.
|
| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
2556. |
| Subjects: |
| Abstract: | The compressive stress for buckling is calculated for a rectangular flat sandwich plate with loaded edges simply supported and unloaded edges rigidly clamped. in the calculations Hoff's differential equations are integrated by Legget's method to obtain lower bounds and by Galerkin's method to establish upper bounds. True values of the buckling stress are estimated as arithmetic means of these bounds and are presented in a diagram which covers the entire practical range of the geometric and mechanical quantities involved. |
|---|---|
| Item Description: | "January 1952." NACA TN Number 2556. |
| Physical Description: | 66 pages : illustrations ; 28 cm. |
| Bibliography: | Includes bibliographical references. |
| Action Note: | committed to retain 20230101 20480101 Alliance Shared Trust https://www.coalliance.org/shared-print-archiving-policies. |