MEYER et al., 1963 - Google Patents
Conical segment method for analyzing open crown shells of revolution for edge loadingMEYER et al., 1963
- Document ID
- 15777765668557896230
- Author
- MEYER R
- HARMON M
- Publication year
- Publication venue
- AIAA Journal
External Links
Snippet
FOR many years investigators have directed their activities toward solving the shell equations to obtain the edge solutions for various shells of revolution. 1-7~ 9 Limiting sequences used to obtain a solution can be defined in a variety of ways. The sequence may …
- 238000004458 analytical method 0 abstract description 19
Similar Documents
Publication | Publication Date | Title |
---|---|---|
MEYER et al. | Conical segment method for analyzing open crown shells of revolution for edge loading | |
Sun et al. | Equivalent analysis and failure prediction of quasi-isotropic composite sandwich cylinder with lattice core under uniaxial compression | |
Calladine | Understanding imperfection-sensitivity in the buckling of thin-walled shells | |
Bushnell et al. | Finite-difference energy method for nonlinear shell analysis | |
Lopatin et al. | Axial deformability of the composite lattice cylindrical shell under compressive loading: Application to a load-carrying spacecraft tubular body | |
Błachut et al. | On buckling of toroidal shells under external pressure | |
Elham et al. | Tool for preliminary structural sizing, weight estimation, and aeroelastic optimization of lifting surfaces | |
Navaratna et al. | Stability analysis of shells of revolution by the finite-element method. | |
Daghighi et al. | Bend-free design of super ellipsoids of revolution composite pressure vessels | |
Bushnell | Nonlinear axisymmetric behavior of shells of revolution. | |
Calladine | Paper 11: A Rapid Method for Estimating the Greatest Stress in a Structure Subject to Creep | |
Becker | Handbook of Structural Stability: Part 2-Buckling of Composite Elements | |
Crawford et al. | Minimum weight potentials for stiffened plates and shells | |
Simitses | Instability of orthotropic cylindrical shells under combined torsionand hydrostatic pressure. | |
Shanygin et al. | Main benefits of pro-composite layouts for wing and fuselage primary structure units | |
Dung et al. | Nonlinear stability of functionally graded material (FGM) sandwich cylindrical shells reinforced by FGM stiffeners in thermal environment | |
Kadoli et al. | A theoretical analysis of linear thermoelastic buckling of composite hemispherical shells with a cut-out at the apex | |
Senjanović et al. | Buckling analysis of toroidal shell by Rayleigh-Ritz method | |
Almroth et al. | Buckling of shells of revolution with various wall constructions. Volume 1-Numerical results | |
Goldfeld | Elastic buckling and imperfection sensitivity of generally stiffened conical shells | |
Heard Jr et al. | Design, Analysis, and Tests of a Structural Prototype Viking Aeroshell | |
Felton et al. | Optimized components in truss synthesis. | |
Semenyuk | Stability of corrugated arches under external pressure | |
Johns | Theoretical elastic mismatch stresses | |
Crichlow et al. | The analysis of redundant structures by the use of high-speed digital computers |