A comprehensive model of anisotropic multilayered double curved shells fulfilling a priori the interlaminar continuity requirements for the transverse shear and transverse normal stress as well as the static conditions on the bounding surfaces of the shell is developed in this paper. To this end, Reissner’s mixed variational theorem is employed to derive the equations governing the dynamic equilibrium and compatibility of each layer, while the interlaminar continuity conditions are used to drive the equations at the multilayered level. No assumptions have been made concerning the terms of type thickness to radii shell ratio h/R. Classical displacement formulations and related equivalent single layer equations have been derived for comparison purposes. Comparison of frequency predictions based upon the presented structural model with a number of results spread throughout the specialized literature and obtained via other models reveals that this advanced model provides results in excellent agreement with the ones based on three-dimensional elasticity theory, and better as compared to the ones violating the interlaminar stress continuity requirements and/or transverse normal stress and related effects.
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March 1999
Technical Papers
A Reissner’s Mixed Variational Theorem Applied to Vibration Analysis of Multilayered Shell
E. Carrera
E. Carrera
Department of Aeronautics and Aerospace Engineering, Politecnico di Torino, Corso Duca degli Abruzzi, 24, 10129 Torino, Italy
e-mail: carrera@polito.it
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E. Carrera
Department of Aeronautics and Aerospace Engineering, Politecnico di Torino, Corso Duca degli Abruzzi, 24, 10129 Torino, Italy
e-mail: carrera@polito.it
J. Appl. Mech. Mar 1999, 66(1): 69-78 (10 pages)
Published Online: March 1, 1999
Article history
Received:
April 1, 1998
Revised:
June 17, 1998
Online:
October 25, 2007
Citation
Carrera, E. (March 1, 1999). "A Reissner’s Mixed Variational Theorem Applied to Vibration Analysis of Multilayered Shell." ASME. J. Appl. Mech. March 1999; 66(1): 69–78. https://doi.org/10.1115/1.2789171
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