Published: Jan 1990
| ||Format||Pages||Price|| |
|PDF (1.6M)||43||$25||  ADD TO CART|
|Complete Source PDF (14M)||43||$103||  ADD TO CART|
A mathematical model based on the Euler-Bernoulli beam theory is proposed for predicting the effective Young's moduli of piecewise isotropic composite laminates with local ply curvatures in the main load-carrying layers. Strains in corrugated layers, in-phase layers, and out-of-phase layers are predicted for various geometries and material configurations by assuming matrix layers as elastic foundations of different spring constants.
The effective Young's moduli measured from corrugated aluminum specimens and aluminum/epoxy specimens with in-phase and out-of-phase wavy patterns coincide very well with the model predictions. Moire fringe analysis of an in-phase specimen and an out-of-phase specimen are also presented, confirming the main assumption of the model related to the elastic constraint due to the matrix layers. The present model is also compared with the experimental results and other models, including the microbuckling models, published in the literature.
The results of the present study show that even a very small-scale local ply curvature produces a noticeable effect on the mechanical constitutive behavior of a laminated composite.
composite materials, laminated composites, main load-carrying layer, wavy patterns, local ply curvature, corrugated beam, in-phase, out-of-phase, effective Young's modulus, pseudostrain, tension, compression, shear mode buckling, moire interferometry, moire fringe pattern
Research assistant, Texas A & M University, College Station, TX
Head, Fracture and Fatigue Branch, NASA Langley Research Center, Hampton, VA
Paper ID: STP24130S