10th Edition

ISBN: 9780134319650

Author: Russell C. Hibbeler

Publisher: PEARSON

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Any functioning component, such as machine parts, structural members, pressure vessels, and so on, are all under the influence of more than one force. When anybody is under the influence of more than one force such as shear forces, bending moments, axial…

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Textbook Question

Chapter 4.2, Problem 4.3P

The composite shaft, consisting of aluminum, copper, and steel sections, is subjected to the loading shown. Determine the displacement of end A with respect to end D and the normal stress in each section. The cross-sectional area and modulus of elasticity for each section are shown in the figure. Neglect the size of the collars at B and C.

Chapter 4.2, Problem 4.3P, The composite shaft, consisting of aluminum, copper, and steel sections, is subjected to the loading

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Chapter 4.2, Problem 4.2P

Chapter 4.2, Problem 4.4P

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4.3 The composite shaft, consisting of aluminum, copper, and steel sections, is subjected to the loading shown. Determine the displacement of end A with respect to end D and the normal stress in each section. The cross-sectional area and modulus of elasticity for each section are shown in the figure. Neglect the size of the collars at Band C. 3.50 kip 1.75 kip 1.50 kip 2.00 kip Steel BL 3.50 kip 1.75 kip Aluminum Copper Est = 29 (10)³ Ksi -18 in- -12 in- -16 in- Ecu = 18 (10)3 Ksi ABC = 0.12 in? Eal = 10(10)³ Ksi AcD = 0.09 6in² = 0.09 in? AAB

1. The composite shaft, consisting of aluminum, copper, and steel sections, is subjected to the loading shown. Determine the displacement of B with respect to C and the normal stress in each section. The cross-sectional area and modulus of elasticity for each section are shown in the figure. Neglect the size of the collars at B and C. Aluminum Eal = 70 GPa AAB = 58 mm² 9 kN A Copper Ecu = 126 GPa ABC = 77 mm² 450 mm 16 kN 斤。 16 kN -300 mm BL Steel Est = 200 GPa ACD = 39 mm² 8 kN 8 kN -400 mm 7 kN

Using direct stiffness method determine the nodal displacement of stepped bar as shown in the figure. Also detemine rection support and stresses in each element. Take E= 200GPA 40 mm 15 mm 30 mm 15 kN 200 mm 500 mm 200 mm

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