NASA NTRS · 19930005294
Reliability of stiffened structural panels: Two examples
Abstract
The reliability of two graphite-epoxy stiffened panels that contain uncertainties is examined. For one panel, the effect of an overall bow-type initial imperfection is studied. The size of the bow is assumed to be a random variable. The failure mode is buckling. The benefits of quality control are explored by using truncated distributions. For the other panel, the effect of uncertainties in a strain-based failure criterion is studied. The allowable strains are assumed to be random variables. A geometrically nonlinear analysis is used to calculate a detailed strain distribution near an elliptical access hole in a wing panel that was tested to failure. Calculated strains are used to predict failure. Results are compared with the experimental failure load of the panel.
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Stroud, W. Jefferson, Davis, D. Dale, Jr., Maring, Lise D., Krishnamurthy, Thiagaraja, Elishakoff, Isaac. 1992-12-01. Reliability of stiffened structural panels: Two examples. https://ntrs.nasa.gov/citations/19930005294
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