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A tensile member of 2024-0 aluminum alloy used for aircraft

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Reference no: EM13345187

A tensile member of 2024-0 aluminum alloy used for aircraft fuselage had an original cross-sectional area of 4.0square inches. If the strain hardening exponent, n=0.21 and the strength coefficient Q=56,000 psi, determine:
a) The maximum load that can be carried by the member?
b) The change in length of the member assuming an original length of 4.0 feet? 

Reference no: EM13345187

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