Modal and aeroelastic analysis of trapezoidal corrugated-core sandwich panels in supersonic flow
Authors:
- Wenzheng ZhuangWZWenzheng Zhuang
- Chao YangCYChao Yang
- Zhigang WuZWZhigang Wu
- 1 July 2019
- journal article
- research article
- Published by Elsevier in International Journal of Mechanical Sciences
- Vol. 157-158, 267-281
Abstract
No abstract availableKeywords
This publication has 45 references indexed in Scilit:
- Active aeroelastic flutter analysis and vibration control of supersonic composite laminated plateComposite Structures, 2012
- Flutter of rectangular composite plates with variable fiber pacingComposite Structures, 2011
- Corrugated laminate homogenization modelComposite Structures, 2010
- A Survey With Numerical Assessment of Classical and Refined Theories for the Analysis of Sandwich PlatesApplied Mechanics Reviews, 2008
- Homogenization of corrugated core sandwich panelsComposite Structures, 2003
- Review of Nonlinear Panel Flutter at Supersonic and Hypersonic SpeedsApplied Mechanics Reviews, 1999
- Nonlinear Flutter of Composite Panels Under Yawed Supersonic Flow Using Finite ElementsAIAA Journal, 1999
- Transverse shear stiffness of structural core sandwichComposite Structures, 1994
- An evaluation of equivalent-single-layer and layerwise theories of composite laminatesComposite Structures, 1993
- Panel flutter - A review of the aeroelastic stability of plates and shellsAIAA Journal, 1970