A cylindrical 2014-T6 aluminum alloy bar is subjected to compression-tension stress cycling along its axis; results of

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A cylindrical 2014-T6 aluminum alloy bar is subjected to compression-tension stress cycling along its axis; results of these tests are shown in Figure 8.20. If the bar diameter is 12.0 mm, calculate the maximum allowable load amplitude (in N) to ensure that fatigue failure will not occur at 107 cycles. Assume a factor of safety of 3.0, data in Figure 8.20 were taken for reversed axial tension-compression tests, and that S is stress amplitude?

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Materials Science and Engineering An Introduction

ISBN: 978-1118324578

9th edition

Authors: William D. Callister Jr., David G. Rethwisch

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