The nonlinear post-buckling response of sandwich panels based on the extended high-order sandwich panel theory (EHSAPT) is presented. The model includes the transverse compressibility, the axial rigidity, and the shear effect of the core. Both faces and core are considered undergoing large displacements with moderate rotations. Based on the nonlinear weak form governing equations, the post-buckling response is obtained by the arc-length continuation method together with the branch switching technique. Also, the post-buckling response with imperfections is studied. The numerical examples discuss the post-buckling response corresponding to global buckling and wrinkling. It is found that due to the interaction between faces and core, localized effects may be easily initiated by imperfections after the sandwich structure has buckled globally. Furthermore, this could destabilize the post-buckling response. The post-buckling response verifies the critical load and buckling mode given by the buckling analysis in part I. The axial rigidity of the core, although it is very small compared to that of the faces, has a significant effect on the post-buckling response.
Skip Nav Destination
Article navigation
August 2018
Research-Article
Nonlinear Stability Analysis of Sandwich Wide Panels—Part II: Postbuckling Response
Zhangxian Yuan,
Zhangxian Yuan
School of Aerospace Engineering,
Georgia Institute of Technology,
Atlanta, GA 30332-0150
Georgia Institute of Technology,
Atlanta, GA 30332-0150
Search for other works by this author on:
George A. Kardomateas
George A. Kardomateas
Professor
School of Aerospace Engineering,
Georgia Institute of Technology,
Atlanta, GA 30332-0150
School of Aerospace Engineering,
Georgia Institute of Technology,
Atlanta, GA 30332-0150
Search for other works by this author on:
Zhangxian Yuan
School of Aerospace Engineering,
Georgia Institute of Technology,
Atlanta, GA 30332-0150
Georgia Institute of Technology,
Atlanta, GA 30332-0150
George A. Kardomateas
Professor
School of Aerospace Engineering,
Georgia Institute of Technology,
Atlanta, GA 30332-0150
School of Aerospace Engineering,
Georgia Institute of Technology,
Atlanta, GA 30332-0150
Contributed by the Applied Mechanics Division of ASME for publication in the JOURNAL OF APPLIED MECHANICS. Manuscript received February 21, 2018; final manuscript received April 5, 2018; published online June 1, 2018. Editor: Yonggang Huang.
J. Appl. Mech. Aug 2018, 85(8): 081007 (9 pages)
Published Online: June 1, 2018
Article history
Received:
February 21, 2018
Revised:
April 5, 2018
Citation
Yuan, Z., and Kardomateas, G. A. (June 1, 2018). "Nonlinear Stability Analysis of Sandwich Wide Panels—Part II: Postbuckling Response." ASME. J. Appl. Mech. August 2018; 85(8): 081007. https://doi.org/10.1115/1.4039954
Download citation file:
Get Email Alerts
Related Articles
Nonlinear Stability Analysis of Sandwich Wide Panels—Part I: Buckling Behavior
J. Appl. Mech (August,2018)
Numerical Stability Criteria for Localized Post-buckling Solutions in a Strut-on-Foundation Model
J. Appl. Mech (May,2004)
Instability of Incompatible Bilayered Soft Tissues and the Role of Interface Conditions
J Biomech Eng (October,2019)
Bifurcations of Equilibria in Potential Systems at Bimodal Critical Points
J. Appl. Mech (March,2008)
Related Chapters
Deformation and Stability of Gold/Polysilicon Layered MEMS Plate Structures Subjected to Thermal Loading
Mechanical Properties of Structural Films
Dynamic Behavior in a Singular Delayed Bioeconomic Model
International Conference on Instrumentation, Measurement, Circuits and Systems (ICIMCS 2011)
Two-Dimension Simulation of a Red Blood Cell Partitioning in Microvascular Bifurcation
International Conference on Software Technology and Engineering (ICSTE 2012)