Critical combinations of torsion and direct axial stress for thin-walled cylinders
An edition of Critical combinations of torsion and direct axial stress for thin-walled cylinders (1947)
By S. B. Batdorf
Publish Date
1947
Publisher
National Advisory Committee for Aeronautics
Language
eng
Pages
28
Description:
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.
subjects: Shells (Engineering), Thin-walled structures, Cylinders, Strains and stresses, Torsion, Buckling (Mechanics), Coques (Ingénierie), Structures à parois minces, Cylindres, Contraintes (Mécanique), Torsion (Mécanique), Flambage (Résistance des matériaux), Shell structures, Cylinders (solids), Torsional stress