journal article·1997-06

Thermostructural Finite Element Analysis of Laminated Doubly Curved Composite Shells

D. Maruthi Rao, P. K. Sinha

Publisher page

Abstract

The present investigation concerns with the development of a finite element method for the thermostructural analysis of laminated doubly curved composite shells. The thermal analysis includes all conventional modes of heat transfer including external heat fluxes and convection environments. The shell strain-deformation relations are based on Donnell's shallow shell theory. The thermo-mechanical properties of composites are assumed to be temperature dependent. Both steady and transient states are analysed. The present results are found to compare well with those existing in the open literature. Numerical results are also obtained for displacements and stresses to study the effects of thermal boundary conditions, radius to span ratios, stacking sequences, structural boundary conditions and temperature dependent material properties.
Source: crossref · Quality: baseline

Research context

OpenAlex topics: Composite Structure Analysis and Optimization · Mechanical Engineering and Vibrations Research · Topology Optimization in Engineering

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

Affiliations

Department of Aerospace Engineering, Indian Institute of Technology, Kharagpur 721 302, India

References (12)

Show source-provided references
1. Boley, B. A. · 1960
2. Nowacki, W. · 1962
3. 10.1007/978-3-7091-8447-910.1007/978-3-7091-8447-9 ↗
4. Keene, F. W. · J. Thermal Stresses, · 1990 · 13 · 34310.1080/01495739008927043 ↗
5. 10.1115/1.342376210.1115/1.3423762 ↗
6. 10.1016/0045-7949(88)90204-010.1016/0045-7949(88)90204-0 ↗
7. 10.1016/0045-7949(94)90086-810.1016/0045-7949(94)90086-8 ↗
8. Krysko, V. A. · Prikladanya Mekhanika, · 1986 · 22 · 409
9. Lukasiewicz, S. A. · 1988
10. 10.1016/0266-3538(94)90049-310.1016/0266-3538(94)90049-3 ↗
11. 10.1016/0045-7949(89)90051-510.1016/0045-7949(89)90051-5 ↗
12. 10.1080/0149573800892697510.1080/01495738008926975 ↗