Compressive buckling of simply supported curved plates and cylinders of sandwich construction
By: Manuel Stein and J. Mayers
Contributors: Mayers, J.; United States. National Advisory Committee for Aeronautics
Series: National Advisory Committee for Aeronautics -- no. 2601; Technical note (United States. National Advisory Committee for Aeronautics) -- no. 2601.
Publisher: National Advisory Committee for Aeronautics
Published: 1952
Place of publication: Washington, D.C
Language: eng
Number of pages: 34
ISBN-13: 9781680156232
Subjects: Plates (Engineering); Curvature; Cylinders; Sandwich construction; Buckling (Mechanics); Loads (Mechanics); Strains and stresses; Cylindres; Construction sandwich; Flambage (Résistance des matériaux); Charges; Contraintes (Mécanique); Cylinders (solids); Buckling; Warping; Stress; Strain
Description: Theoretical solutions are presented for the buckling in uniform axial compression of two types of simply supported curved sandwich plates: the corrugated-core type and the isotropic type. Results are given in the form of equations and curves.
Notes: "January 1952."

NACA TN No. 2601.

Includes bibliographical references.