A solid brass [E = 98 GPa] axial member is loaded and supported as shown. Segments (1) and (2) each have a diameter of 26 mm and segment (3) has a diameter of 12 mm. Assume L1 = 1.9 m, L2 = 1.3 m, L3 = 1.5 m, R = 40 kN, Q = 12 kN, and P = 22 kN. (a) Determine the axial force in section (1) section (2) and section (3) in kN. and the axial deformation of section (2) (b) Determine the deflection of joint D (positive if downward) with respect to the fixed support at A. in mm. (c) Determine the maximum normal stress in the entire axial member. Give answer in MPa.
A solid brass [E = 98 GPa] axial member is loaded and supported as shown. Segments (1) and (2) each have a diameter of 26 mm and segment (3) has a diameter of 12 mm. Assume L1 = 1.9 m, L2 = 1.3 m, L3 = 1.5 m, R = 40 kN, Q = 12 kN, and P = 22 kN. (a) Determine the axial force in section (1) section (2) and section (3) in kN. and the axial deformation of section (2) (b) Determine the deflection of joint D (positive if downward) with respect to the fixed support at A. in mm. (c) Determine the maximum normal stress in the entire axial member. Give answer in MPa.
Refrigeration and Air Conditioning Technology (MindTap Course List)
8th Edition
ISBN:9781305578296
Author:John Tomczyk, Eugene Silberstein, Bill Whitman, Bill Johnson
Publisher:John Tomczyk, Eugene Silberstein, Bill Whitman, Bill Johnson
Chapter50: Commercial, Packaged Rooftop, Variable Refrigerant Flow, And Variable Air Volume Systems
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A solid brass [E = 98 GPa] axial member is loaded and supported as shown. Segments (1) and (2) each have a diameter of 26 mm and segment (3) has a diameter of 12 mm. Assume L1 = 1.9 m, L2 = 1.3 m, L3 = 1.5 m, R = 40 kN, Q = 12 kN, and P = 22 kN.
(a) Determine the axial force in section (1) section (2) and section (3) in kN. and the axial deformation of section (2)
(b) Determine the deflection of joint D (positive if downward) with respect to the fixed support at A. in mm.
(c) Determine the maximum normal stress in the entire axial member. Give answer in MPa.
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