Accession Number : ADA302390

Title :   Evaluation of a Hybrid, Anisotropic, Multilayered, Quadrilateral Finite Element.

Descriptive Note : Technical paper,

Corporate Author : NATIONAL AERONAUTICS AND SPACE ADMINISTRATION HAMPTON VA LANGLEY RESEARCH CEN TER

Personal Author(s) : Robinson, James C. ; Blackburn, Charles L.

PDF Url : ADA302390

Report Date : AUG 1978

Pagination or Media Count : 32

Abstract : A hybrid, anisotropic, multilayered, quadrilateral finite element with bending-extensional coupling is evaluated.

Descriptors :   *STRESS ANALYSIS, *LAMINATES, *FINITE ELEMENT ANALYSIS, MATHEMATICAL MODELS, HIGH TEMPERATURE, STRUCTURAL ANALYSIS, BEAMS(STRUCTURAL), STIFFNESS, DISPLACEMENT, FIBER REINFORCED COMPOSITES, COMPOSITE STRUCTURES, SHELLS(STRUCTURAL FORMS), PLATES, APPROXIMATION(MATHEMATICS), SHEAR STRESSES, BUCKLING, THERMAL STRESSES, BENDING STRESS.

Subject Categories : Laminates and Composite Materials
      Numerical Mathematics
      Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE