Ушбу ишга иқтибос қилган ишлар

2 та иш

Иш: Accurate Response of Wing Structures to Free-Vibration, Load Factors, and Nonstructural Masses

1. Effect of different geometrically nonlinear strain measures on the static nonlinear response of isotropic and composite shells with constant curvature

   A. Pagani, R. Azzara, Bin Wu +1

   ПрепринтComposite Structure Analysis and OptimizationarXiv (Cornell University)20210 иқтибос

   ABIABI:AkademIndex/openalex/2021.preprint.000112

2. Buckling and post-buckling of anisotropic at panels subjected to axial and shear in-plane loadings accounting for classical and refined structural and nonlinear theories

   Erasmo Carrera, R. Azzara, Ehsan Daneshkhah +2

   ПрепринтComposite Structure Analysis and OptimizationarXiv (Cornell University)20210 иқтибос

   ABIABI:AkademIndex/openalex/2021.preprint.000114