Accession Number : ADA307525
Title : Structural Behavior and Buckling Strength of Honeycomb Sandwich Cylinders Subjected to Bending.
Descriptive Note : Technical note,
Corporate Author : NATIONAL AERONAUTICS AND SPACE ADMINISTRATION HAMPTON VA LANGLEY RESEARCH CEN TER
Personal Author(s) : Peterson, James P. ; Anderson, James K.
PDF Url : ADA307525
Report Date : AUG 1965
Pagination or Media Count : 29
Abstract : Results of buckling tests on three honeycomb sandwich cylinders loaded in bending are presented and discussed. In addition, analytical studies are made on (1) the influence of the core and bonding material in enhancing the stiffness of composite sandwich plates like those of the walls of the test cylinders and on (2) plastic buckling of sandwich cylinders in compression. Results of the two studies are compared with observed behavior of the test cylinders. The bending stiffness of the test cylinders correlated well with predicted behavior. Buckling of the test cylinders occurred at lower loads than predicted by theory by about the same margin that would be suggested by an extrapolation of the results of buckling tests on conventional thin-wall cylinders.
Descriptors : *COMPOSITE MATERIALS, *BENDING, *BUCKLING, *SANDWICH CONSTRUCTION, PLASTIC DEFORMATION, LOAD DISTRIBUTION, ALUMINUM ALLOYS, STRUCTURAL ANALYSIS, STIFFNESS, MODULUS OF ELASTICITY, COMPOSITE STRUCTURES, STRENGTH(MECHANICS), CYLINDRICAL BODIES, PLATES, WALLS, BONDING, FAILURE(MECHANICS), ADHESIVES, AXIAL LOADS, HONEYCOMB STRUCTURES.
Subject Categories : Laminates and Composite Materials
Solid State Physics
Distribution Statement : APPROVED FOR PUBLIC RELEASE