Critical combinations of torsion and direct axial stress for thin-walled cylinders /
| Main Author: | |
|---|---|
| Corporate Authors: | , |
| Other Authors: | , |
| Format: | eBook |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1947.
|
| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
no. 1345. |
| Subjects: | |
| Online Access: | Connect to the full text of this electronic book |
| Abstract: | A theoretical solution is presented for the determination of the combinations of direct axial stress and torsion which cause thin-walled cylinders with either simply supported or clamped edges to buckle. This theoretical solution is used in conjunction with available test data to develop empirical curves and formulas for use in design. Comparisons are made with theoretical and empirical solutions obtained in other investigations. |
|---|---|
| Item Description: | "June 1947." NACA TN Number 1345. Electronic resource. |
| Physical Description: | 1 online resource (28 pages, 8 unnumbered pages) : illustrations, tables. |
| Bibliography: | Includes bibliographical references. |
| ISBN: | 9781680156058 1680156055 |