Nonlinear Vibrations of FGM Cylindrical Panel with Simply Supported Edges in Air Flow
Chaotic and periodic motions of an FGM cylindrical panel in hypersonic flow are investigated. The cylindrical panel is also subjected to in-plane external loads and a linear temperature variation in the thickness direction. The temperature dependent material properties of panel which are assumed to...
Saved in:
Main Authors: | Y. X. Hao, W. Zhang, S. B. Li, J. H. Zhang |
---|---|
Format: | Article |
Language: | English |
Published: |
Wiley
2015-01-01
|
Series: | International Journal of Aerospace Engineering |
Online Access: | http://dx.doi.org/10.1155/2015/246352 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Large Deformation Elastic Analysis of Pressurized FGM Thick Cylindrical Shells with Nonlinear Plane Elasticity Theory (NPET)
by: Navid Bahadorani, et al.
Published: (2025-04-01) -
An Investigation on the Nonlinear Free Vibration Analysis of Beams with Simply Supported Boundary Conditions Using Four Engineering Theories
by: R. A. Jafari-Talookolaei, et al.
Published: (2011-01-01) -
Free Vibration of Partially Supported Cylindrical Shells
by: S. Mirza, et al.
Published: (1995-01-01) -
Vibration Analysis of Reinforced Concrete Simply Supported Beam versus Variation Temperature
by: Hanbing Liu, et al.
Published: (2017-01-01) -
Vibrations of a Simply Supported Beam with a Fractional Viscoelastic Material Model – Supports Movement Excitation
by: Jan Freundlich
Published: (2013-01-01)