Check nearby libraries
Buy this book
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.
Check nearby libraries
Buy this book
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 stressEdition | Availability |
---|---|
1
Critical combinations of torsion and direct axial stress for thin-walled cylinders
1947, National Advisory Committee for Aeronautics
in English
1680156055 9781680156058
|
aaaa
|
Book Details
Edition Notes
"Langley Memorial Aeronautical Laboratory."
Date of issue: June 1947.
Report no. NACA TN No. 1345.
Includes bibliographical references (page 25)
Classifications
The Physical Object
ID Numbers
Community Reviews (0)
December 19, 2022 | Created by MARC Bot | import new book |