A non-linear finite element analysis including a new flat shell element has been developed to examine the response of laminated panels going through large deflections and rotations under uniform temperature change. The equilibrium path describing the relationship between temperature and deflection i
A model of passive thermal nondestructive evaluation of composite laminates
β Scribed by John A. Charles; Dale W. Wilson
- Publisher
- Society for Plastic Engineers
- Year
- 1981
- Tongue
- English
- Weight
- 680 KB
- Volume
- 2
- Category
- Article
- ISSN
- 0272-8397
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β¦ Synopsis
Abstract
A numerical model of passive thermal nondestructive evaluation (NDE) of composite laminates was developed. This model, based on a transient, threeβdimensional, finite difference solution to the heat conduction equations, can be used to characterize inβplane defects in the laminates and to predict the laminate response to the thermal test. The model was experimentally verified using two material systems. A parametric study was then conducted to ascertain which variables were critical to the success of passive thermal NDE, and how flaw resolution might be improved.
π SIMILAR VOLUMES
Thermal buckling analysis of laminated composites is presented by using a layer-wise theory. Governing buckling equations are derived from the variational principle and a finite element method is developed to formulate the problem. Numerical results are obtained and compared with those of other theo