Handbook of structural stability
Subtitle: Buckling of composite elements
By: Herbert Becker
Contributors: United States. National Advisory Committee for Aeronautics
Series: Technical note / National Advisory Committee for Aeronautics -- 3782; Technical note (United States. National Advisory Committee for Aeronautics) -- no. 3782.
Publisher: National Advisory Committee for Aeronautics
Published: 1957
Place of publication: Washington, D.C
Language: eng
Number of pages: 72
ISBN-13: 9781680156270
Subjects: Structural analysis (Engineering); Stability; Columns; Cylinders; Buckling (Mechanics); Loads (Mechanics); Strains and stresses; Théorie des constructions; Stabilité; Cylindres; Flambage (Résistance des matériaux); Charges; Contraintes (Mécanique); Structural analysis; Cylinders (solids)
Description: The local buckling of stiffener sections and the buckling of plates with sturdy stiffeners are reviewed, and the results are summarized in charts and tables. Numerical values of buckling coefficients are presented for longitudinally compressed stiffener sections of various shapes, for stiffened plates loaded in longitudinal compression and in shear, and for stiffened cylinders loaded in torsion. Although the data presented consist primarily of elastic-buckling coefficients, the effects of plasticity are discussed for a few special cases.
Notes: NACA TN No. 3782.

Includes bibliographical references.