General higher-order equivalent single layer theory for free vibrations of doubly-curved laminated composite shells and panels

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An equivalent layer-wise approach for the free vibration analysis of thick and thin laminated and sandwich shells (2016, methodology): “For this purp se, the laminated conical shell described in the works [61,83] is considered.”
Stress and strain recovery for functionally graded free-form and doubly-curved sandwich shells using higher-order equivalent single layer theory (2015, background): “sth order vector of the stress resultants and A(ss) is the matrix of the elastic constants [148,150] defined as”
Static analysis of functionally graded conical shells and panels using the generalized unconstrained third order theory coupled with the stress recovery (2014, methodology): “With the in-plane stress components indirectly derived from the GDQ-solution [54–92] of the fundamental system, the integration of the three dimensional indefinite equilibrium equations is carried out.”