Zobrazeno 1 - 10
of 64
pro vyhledávání: '"Johann Arbocz"'
Autor:
Yiska Goldfeld, Johann Arbocz
Publikováno v:
Thin-Walled Structures ISBN: 9781351077309
Thin-Walled Structures
Thin-Walled Structures
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e84ef4172bea9154d242ce6bd7271300
https://doi.org/10.1201/9781351077309-82
https://doi.org/10.1201/9781351077309-82
Autor:
Johann Arbocz, Ronald P. Notenboom
Publikováno v:
AIAA Journal. 49:695-702
The Sanders shell equations for imperfect anisotropic circular cylindrical shells are used for the development of a research tool to study the nonlinear interaction of circumferential waves under different loading conditions. Therefore, a truncated F
Publikováno v:
International Journal of Structural Stability and Dynamics. 10:623-644
The discrepancy between the analytically determined buckling load of perfect cylindrical shells and experimental test results is traced back to imperfections. The most frequently used guideline for design of cylindrical shells, NASA SP-8007, proposes
Autor:
Johann Arbocz, Yiska Goldfeld
Publikováno v:
Journal of Engineering Mechanics. 132:1335-1344
A hierarchical high-fidelity analysis procedure is adopted for predicting the critical buckling load of filament wound laminated conical shells. This hierarchical procedure includes three levels of fidelity for the analysis. Level-1 assumes that the
Autor:
Mark W. Hilburger, Johann Arbocz
Publikováno v:
AIAA Journal. 43:1823-1827
A probability-based analysis method for predicting buckling loads of compression-loaded laminated composite shells is presented, and its potential as a basis for a new shell-stability design criterion is demonstrated and discussed. In particular, a d
Autor:
James H. Starnes, Johann Arbocz
Publikováno v:
Journal of Aerospace Engineering. 18:168-178
A hierarchical high-fidelity analysis methodology for predicting the critical buckling load of compression-loaded thin-walled isotropic shells is described. This hierarchical procedure includes three levels of fidelity for the analysis. Level 1 assum
Publikováno v:
Structural and Multidisciplinary Optimization. 30:128-141
Optimum laminate configuration for minimum weight of filament-wound laminated conical shells is investigated subject to a buckling load constraint. In the case of a composite laminated conical shell, due to the manufacturing process, the thickness an
Publikováno v:
Thin-Walled Structures. 43:107-133
Optimum laminate configuration for the maximum buckling load of filament-wound laminated conical shells is investigated. In the case of a laminated conical shell, the thickness and the ply orientation (the design variables) are functions of the shell
Autor:
Johann Arbocz, Yiska Goldfeld
Publikováno v:
AIAA Journal. 42:642-649
The buckling behavior of filament-wound laminated conical shell is thoroughly investigated by consideration of the variation of the stiffness coefficients. To date, all analyses of laminated conical shells have been undertaken with constant stiffness
Autor:
James H. Starnes, Johann Arbocz
Publikováno v:
Thin-Walled Structures. 40:729-754
Recent advances in structural analysis and design technology for buckling-critical shell structures are discussed. These advances include a hierarchical analysis strategy that includes analyses that range from classical analysis methods to high-fidel