Statics and Mechanics of Materials (5th Edition)
5th Edition
ISBN: 9780134382593
Author: Russell C. Hibbeler
Publisher: PEARSON
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Textbook Question
Chapter 13.2, Problem 20P
The plate has a thickness of 20 mm and the force P = 3 kN acts along the centerline of this thickness such that d = 150 mm. Plot the distribution of normal stress acting along section a–a.
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Determine the shortest distance d to the edge of the plate at which the force P can be applied so that it produces no compressive stresses in the plate at section a–a. The plate has a thickness of 10 mm and P acts along the centerline of this thickness.
Chapter 13 Solutions
Statics and Mechanics of Materials (5th Edition)
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- The plate has a thickness of 20 mm and width s = 260 mm. Force P acts along the centerline of this thickness. Determine the maximum distance d at which the force P can be applied so that it produces no compressive stresses on the plate at section a-a.arrow_forwardDetermine the maximum distance d to the edge of the plate at which the force P can be applied so that it produces no compressive stresses on the plate at section a–a. The plate has a thickness of 20 mm and P acts along thecenterline of this thickness.arrow_forwardThe box beam is subjected to the 26-kN force that is applied at the center of its width, 75 mm from each side. Determine the principal stresses at point A and show the results in an element located at this point. Use the shear formula to calculate the shear stress.arrow_forward
- The bar has a 100 mm by 15 mm rectangular cross section. The allowable normal and shear stresses on inclined 66° surface a – a must be limited to 50 MPa and 35 MPa, respectively. Determine the 100 mm magnitude of the maximum axial force P that can be applied to the bar, and determine the actual normal and shear Try one stresses acting on inclined plane a – a.arrow_forwardIn each case, the state of stress sx, sy, txy produces normal and shear stress components along section AB of the element that have values of sx = -5 kPa and txy = 8 kPa when calculated using the stress transformation equations.Establish the x and y axes for each segment and specify the angle u, then show these results acting on each segment.arrow_forwardUse Mohr’s circle to determine the normal stress and shear stress acting on the inclined plane AB.arrow_forward
- Determine Value of x if the Normal stress at rod is equal to the stress at rectangular pipe A =400 mm2 F = 8kN Rod A =650 mm2 rectangular Pipearrow_forwardDetermine state of stress at the remaining points (P2, P3 and P4). Calculate the maximumprincipal (σ1) and maximum in-plane stress (τmax) for the remaining points (P2, P3 and P4) located at Point A.arrow_forwardThe vertical force P acts on the bottom of the plate having a negligible weight. Determine the shortest distance d to the edge of the plate at which it can be applied so that it produces no compressive stresses on the plate at section a-a. The plate has a thickness of 10 mm and P acts along the centerline of this thickness. a 200 mm- d 300 mm a 500 mmarrow_forward
- Determine the normal stress and shear stress acting on the inclined plane AB. Solve the problem using the stress transformation equations. Show the results on the sectional element.arrow_forward1) Two wrenches are used to tighten the pipe. If P = 300 N is applied to each wrench, determine the maximum torsional shear stress developed within regions AB and BC. The pipe has an outer diameter of 25 mm and inner diameter of 20 mm. Sketch the shear stress distribution for both cases. 250 mm B 250 mmarrow_forwardThe wide-flange beam is subjected to the 50-kN force. Determine the principal stresses in the beam at point A located on the web at the bottom of the upper flange. Although it is not very accurate, use the shear formula to calculate the shear stress. A B₂ ➜ 10 mm- B 200 mm 12 mm 250 mm 12 mm -3 m 50 kNarrow_forward
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