Thermal buckling analysis of isotropic and composite plates with a hole
- National Taiwan Univ., Taipei (China)
Thermal buckling of both circular isotropic plates and square antisymmetric angle-ply laminates with a hole in the middle, and subject to a uniform temperature rise is analyzed by either closed-form solution for the former or finite-element method for the latter. Thin-plate theory is used to analyze the isotropic plates. However, a high-order displacement theory including high-order terms along the transverse direction taking into account transverse normal strain is used in the case of laminates. Results for the isotropic plates indicate that, in contrast to the reduction in mechanical buckling loads due to the hole, the thermal buckling temperature actually rises as the size of the hole increases, which indicates that the effect on stress reduction exceeds that on stiffness decrease. Results are more complicated for laminated plates, due to anisotropy. 14 refs.
- OSTI ID:
- 6490555
- Journal Information:
- Journal of Thermal Stresses, Journal Name: Journal of Thermal Stresses Vol. 13:3; ISSN 0149-5739; ISSN JTSTD
- Publisher:
- Taylor & Francis
- Country of Publication:
- United States
- Language:
- English
Thermal Buckling of Thick Antisymmetric Angle-Ply Laminates
|
journal | January 1987 |
Thermal buckling of orthotropic cylindrical shells
|
journal | January 1973 |
Thermal Buckling of Orthotropic Cylindrical Shells
|
journal | March 1975 |
Thermal Buckling Analysis of Composite Laminated Plates by the Finite-Element Method
|
journal | January 1989 |
A Simple Higher-Order Theory for Laminated Composite Plates
|
journal | December 1984 |
A High-Order Theory of Plate Deformation—Part 2: Laminated Plates
|
journal | December 1977 |
Similar Records
Thermal buckling of thick antisymmetric angle-ply laminates
Three-dimensional solutions for the free vibrations and buckling of thermally stressed multilayered angle-ply composite plates