Knockdown Factor based on Imperfection Sensitivity Analysis for Stiffened Shells
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[1] David Bushnell,et al. Optimization of composite, stiffened, imperfect panels under combined loads for service in the postbuckling regime , 1993 .
[2] Kim J.R. Rasmussen,et al. Nonlinear buckling optimization of composite structures considering ''worst" shape imperfections , 2010 .
[3] Mark W. Hilburger,et al. Effects of Imperfections on the Buckling Response of Compression-Loaded Composite Shells , 2000 .
[4] Janis Auzins,et al. Surrogate modeling in design optimization of stiffened composite shells , 2006 .
[5] M. Biagi,et al. Reliability-based knockdown factors for composite cylindrical shells under axial compression , 2008 .
[6] G. I. Schuëller,et al. Buckling analysis of cylindrical shells with random geometric imperfections , 2003 .
[7] James H. Starnes,et al. Future directions and challenges in shell stability analysis , 1997 .
[8] Johann Arbocz,et al. The effect of general imperfections on the buckling of cylindrical shells , 1968 .
[9] David Bushnell,et al. Approximate method for the optimum design of ring and stringer stiffened cylindrical panels and shells with local, inter-ring, and general buckling modal imperfections , 1994 .
[10] Luca Lanzi,et al. Post-buckling optimization of composite stiffened panels: Computations and experiments , 2006 .