scholarly journals Imperfection sensitivity of laminated conical shells

2007 ◽  
Vol 44 (3-4) ◽  
pp. 1221-1241 ◽  
Author(s):  
Yiska Goldfeld
Keyword(s):  
Imperfection Sensitivity ◽  
Conical Shells ◽  
Laminated Conical Shells

Design of laminated conical shells using spectral Chebyshev method and lamination parameters

2021 ◽  
pp. 114969
Author(s):  
Peiman Khandar Shahabad ◽  
Mirmeysam Rafiei Anamagh ◽  
Bekir Bediz
Keyword(s):  
Lamination Parameters ◽  
Conical Shells ◽  
Chebyshev Method ◽  
Laminated Conical Shells

scholarly journals The influence of the manufacturing constraints on the optimal design of laminated conical shells

2020 ◽  
Vol 235 ◽  
pp. 111820 ◽  
Author(s):  
Adam Stawiarski ◽  
Małgorzata Chwał ◽  
Marek Barski ◽  
Aleksander Muc
Keyword(s):  
Optimal Design ◽  
Manufacturing Constraints ◽  
Conical Shells ◽  
Laminated Conical Shells

Free Vibration of Axially Loaded Laminated Conical Shells

1999 ◽  
Vol 66 (3) ◽  
pp. 758-763 ◽  
Author(s):  
L. Tong
Keyword(s):  
Free Vibration ◽  
Axial Load ◽  
Governing Equations ◽  
Load Effect ◽  
Critical Buckling Load ◽  
Conical Shells ◽  
Axial Tension ◽  
Axially Loaded ◽  
Constant Axial Load ◽  
Laminated Conical Shells

Analytical solutions for the three displacements are obtained, in the form of power series, directly from the three governing equations for free vibration of laminated conical shells under axial load. Numerical results are presented for free vibration of axially loaded laminated conical shells with different geometric parameters and under two types of boundary conditions. It is found that an axial tension increases the frequencies while an axial compression decreases the frequencies. For the shells studied, the effect of axial load on the lowest frequency of the shell is found to be not sensitive to change in semivertex angle when the applied axial load is kept as a constant fraction of the critical buckling load. However, the axial load effect becomes very sensitive to variation in semivertex angle when a constant axial load is applied.

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