Vibration of Laminated Shells and Plates
By M. Qatu. 2004
567 citations recorded by the source corpus.
Subfields: General Materials Science, Mechanics of Materials
View Paper: https://www.semanticscholar.org/paper/9271c69746ffa2443934112e240e0da521178cc4
How researchers see this paper
The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.
In General Materials Science
- Erasmo Carrera
- Francesco Tornabene
- F. Miglioretti
- Ö. Civalek
- Nicholas Fantuzzi
- Alessandro Ceruti
- Erasmo Viola
- Marco Petrolo
In Mechanics of Materials
- Francesco Tornabene
- Nicholas Fantuzzi
- Erasmo Viola
- Erasmo Carrera
- A. S. Sayyad
- Y. Ghugal
- Salvatore Brischetto
- M. Bacciocchi
Citations in the corpus
- Static analysis of laminated composite curved shells and panels of revolution with a posteriori shear and normal stress recovery using generalized differential quadrature method (2012, methodology): “In order to include the effect of the initial curvature in the evaluation of the stress resultants a generalization of the Classical Reissner–Mindlin Theory (CRMT) has been proposed in literature by Kraus [7], Qatu [16–18] and Toorani and Lakis [19].”
- Selection of appropriate multilayered plate theories by using a genetic like algorithm (2012, methodology): “For a complete overview of existing Layer-Wise and Equivalent Single Layer theories see the excellent reviews by Ambartsumian [3], Librescu and Reddy [4], Grigolyuk and Kulikov [5], Kapania and Raciti [6,7], Kapania [8], Noor [9–11], Reddy and Robbins [12], Carrera [13,14], Qatu [15,16], and the boo”
- Static analysis of doubly-curved anisotropic shells and panels using CUF approach, differential geometry and differential quadrature method (2014, background): “Thin and thick shell topics were studied and widely developed over the last 70 years [1–53].”
- Recent research advances on the dynamic analysis of composite shells: 2000-2009 (2010, methodology): “(2) [1].”
- Three-dimensional free vibration analysis of rotating laminated conical shells: layerwise differential quadrature (LW-DQ) method (2012, background): “and [C̄] = [T ]−1[C][T ] is the transformed stiffness matrix for a laminated shell, in which [C] is the principle material stiffness matrix and [T ] is the transformation matrix [11,12].”