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Question: aircraft structure analysis...

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Aircraft Structure Analysis
P.11.4. The rivet group shown in Fig. P.11.4 connects two narrow lengths of plate one of which carries a 15 kN load positioned as shown. If the ultimate shear strength of a rivet is 350 N/mm2 and its failure strength in compression is 600 N/mm2, determine the minimum allowable values of rivet diameter and plate thickness. Answer: The rivet diameter is 4.2 mm, plate thickness is 1.93 mm
Problems 393 50mm 15kN 2 3 25 mm 6 5 4 25 mm 7 25mm 25mm FIGURE P.11.4
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