
Accession Number : AD0488849
Title : COMPARISON OF SHELL AND ELASTICITY THEORY SOLUTIONS FOR THICK, ORTHOTROPIC, CIRCULAR CYLINDRICAL SHELLS.
Descriptive Note : Research rept.,
Corporate Author : GRUMMAN AIRCRAFT ENGINEERING CORP BETHPAGE NY RESEARCH DEPT
Personal Author(s) : CrouzetPascal, Jacques ; Pifko, Allan
Report Date : SEP 1966
Pagination or Media Count : 49
Abstract : Equations for the static response to arbitrary loads of orthotropic, circular cylindrical shells with thicknesses beyond the thin shell theory range are systematically applied to a number of specific problems. On the basis of comparisons with corresponding results in the theory of elasticity, the range of validity of these equations is established. However, for lack of appropriate exact solutions, the validity of the present equations for orthotropic shells under nonuniform loads must be inferred from isotropic solutions. (Author)
Descriptors : *ELASTIC SHELLS), (*CYLINDRICAL BODIES, THICKNESS, LOADS(FORCES), RESPONSE, ELASTIC PROPERTIES, THEORY, DEFORMATION, STRAIN(MECHANICS), TORSION, SHEAR STRESSES, STRESSES, MATHEMATICAL ANALYSIS, MATRICES(MATHEMATICS), NUMERICAL METHODS AND PROCEDURES, FOURIER ANALYSIS, SERIES(MATHEMATICS), PARTIAL DIFFERENTIAL EQUATIONS.
Subject Categories : Guided Missiles
Mechanics
Distribution Statement : APPROVED FOR PUBLIC RELEASE