A critical machine part in an aircraft flap actuator may be adequately modeled as a solid cylindrical
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A critical machine part in an aircraft flap actuator may be adequately modeled as a solid cylindrical bar subjected to an axial force P of 10,000 lbs, a bending moment A{; = 1500 in-lb, and a torsional moment T= 4000 indb_ If it is proposed to use a 1-inch-diamester bar of 7075-T6 aluminum {0,p = 72,000 psi, o, = 82,000 psi, e = 11 percent in 2 inches), what would be the safely factor on yielding for this member? Give a clear and complete analysis, stating what you are doing at every step.
Related Book For
Income Tax Fundamentals 2013
ISBN: 9781285586618
31st Edition
Authors: Gerald E. Whittenburg, Martha Altus Buller, Steven L Gill
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