StressCheck Tutorial: Planar Modeling of a Skin-Stiffener-Fasteners Assembly
Abstract: Modeling of a Planar skin, stiffener and fasteners (as fastener/link elements) assembly for an in-plane, general nonlinear analysis. In-plane axial loads only, in which the stiffener/skin load ratio is 0.55. Model pre-processing only.
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“In the case of the through crack configuration, the comparison of experimental and StressCheck® derived geometry factors showed a close correlation and were an improvement to solutions provided in AFGROW at the time. Based on the results of this research, StressCheck® pin-loaded lug geometry factors have since been incorporated into the AFGROW software.”
Dr. Alten GrandtPurdue University