Structural efficiency study of graphite-epoxy aircraft rib structures
暂无分享,去创建一个
[1] Garret N. Vanderplaats,et al. CONMIN: A FORTRAN program for constrained function minimization: User's manual , 1973 .
[2] F. W. Williams,et al. Incorporation of Lagrangian Multipliers into an algorithm for finding exact natural frequencies or critical buckling loads , 1983 .
[3] W. J. Stroud,et al. Minimum-Mass Design of Filamentary Composite Panels Under Combined Loads: Design Procedure Based on a Rigorous Buckling Analysis. , 1977 .
[4] W. J. Stroud,et al. Minimum-Mass Design of Filamentary Composite Panels under Combined Loads: Design Procedure Based on Simplified Buckling Equations. , 1976 .
[5] F. W. Williams,et al. Buckling and vibration of anisotropic or isotropic plate assemblies under combined loadings , 1974 .
[6] W. J. Stroud,et al. PASCO: Structural panel analysis and sizing code: Users manual - Revised , 1981 .
[7] W. J. Stroud,et al. PASCO: Structural panel analysis and sizing code, capability and analytical foundations , 1980 .
[8] W. J. Stroud,et al. Buckling loads of stiffened panels subjected to combined longitudinal compression and shear: Results obtained with PASCO, EAL, and STAGS computer programs , 1984 .