Monirul Fernández
Open Access Journal of Engineering Applications · doi:10.55555/oajea.1982.0601.008
Existing standards offer little guidance on steel frame connections as it arises in aircraft structures. In this study nonlinear optimization is employed to investigate the problem under a range of representative conditions. Simplified expressions are shown to be accurate to within 58% for practical purposes. Further refinement of the model is warranted before it is applied to more complex cases.
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