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Accession Number:
AD0488849
Title:
COMPARISON OF SHELL AND ELASTICITY THEORY SOLUTIONS FOR THICK, ORTHOTROPIC, CIRCULAR CYLINDRICAL SHELLS.
Corporate Author:
GRUMMAN AIRCRAFT ENGINEERING CORP BETHPAGE NY RESEARCH DEPT
Report Date:
1966-09-01
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
Descriptive Note:
Research rept.,
Supplementary Note:
Presented at the 5th U.S. National Congress of Applied Mechanics, 14-17 Jun 66, University of Minnesota.
Pages:
0049
Contract Number:
Nonr-3465(00)
File Size:
0.00MB
