Applied Statics and Strength of Materials (6th Edition)
6th Edition
ISBN: 9780133840544
Author: George F. Limbrunner, Craig D'Allaird, Leonard Spiegel
Publisher: PEARSON
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Chapter 19, Problem 19.4P
Compute the allowable tensile load for the double-shear butt joint shown. The plates are equivalent to
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Select the lightest WT4 shape to be used as a 20 ft long tension member to resist the of dead load, D=40 k, live load, L=60 k, snow load, PS=25 k, and earthquake, E=110 k. The connection is two lines of bolts through the flange with three 3/4-in ∅ bolts in each line spaced at 3 in on center. Use A992 Grade 50 steel. Neglect block shear.
Chapter 19 Solutions
Applied Statics and Strength of Materials (6th Edition)
Ch. 19 - Prob. 19.1PCh. 19 - Rework Problem 19.1 assuming a bearing-type...Ch. 19 - Rework Problem 19.1 assuming a bearing-type...Ch. 19 - Compute the allowable tensile load for the...Ch. 19 - Rework Problem 19.4 assuming a bearing-type...Ch. 19 - Rework Problem 19.4 assuming that the bolts are 34...Ch. 19 - Select the number and arrangement of 34 in....Ch. 19 - Calculate the allowable tensile load for the...Ch. 19 - In the connection shown, 14 in. side and end...Ch. 19 - Design the fillet welds parallel to the applied...
Ch. 19 - A fillet weld between two steel plates...Ch. 19 - Design an end connection using longitudinal welds...Ch. 19 - Calculate the allowable tensile load for the butt...Ch. 19 - Calculate the allowable tensile load for the lap...Ch. 19 - Calculate the allowable tensile load for the butt...Ch. 19 - Rework Problem 19.10 assuming that both plates are...Ch. 19 - Rework Problem 19.12 assuming that the angle is an...Ch. 19 - Two ASTM A36 steel plates, each 12 in. by 12 in. ,...Ch. 19 - Rework Problem 19.20 changing the fasteners to 34...Ch. 19 - Calculate the minimum main plate thickness for the...Ch. 19 - A roof truss tension member is made up of 2L6412...Ch. 19 - Rework Problem 19.23 changing the fasteners to six...Ch. 19 - Determine the allowable tensile load that can be...Ch. 19 - The welded connection shown is subjected to an...Ch. 19 - In Problem 19.26, use a 38 in. fillet weld, change...
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- Select the lightest WT4 shape to be used as a 20 ft long tension member to resist the following service loads: dead load, D = 20 k, live load, L = 35 k, snow load, S = 25 k, and earthquake, E = 50 k. The connection is two lines of bolts through the flange with three 3/4-in Ø bolts in each line spaced at 3 in on center. Use A992 Grade 50 steel. Neglect block shear.arrow_forwardThe aircraft link is made from an A992 steel rod. (Figure 1) Figure 1 of 1 18 in.arrow_forwardDetermine the safe tensile load for bolts of (a) M 17 and (b) M 26. Assume that the bolts are not initially stressed and take the safe tensile stress as 305 MPaarrow_forward
- Two parts of a machine, both made from steel, are held together by 5 equally-spaced M6 x 1.0 grade 8.8 bolts that are uniformly tightened to provide a total initial clamping force of 23 kN in the members. Each bolt has a proof stress of 600 MPa, and a tensile area of 20.1 mm². The elasticities are such that the joint constant is 0.2. A uniform static tensile load of 12 kN is applied to the entire joint after it has been preloaded. What is the magnitude of the total clamping force in the joint after the application of the tensile load? Express your answer in units of kilonewtons.arrow_forwardQuestion 3 A typical Can dimensions are given as 63 mm in diameter, 120 mm in height and 0.1 mm thickness. These dimensions were measured on an aluminium beverage can which was carefully cut in half and measured the wall thickness and can diameter. Calculate the critical buckling load for the can and indicate if this is greater than or less than your weight. Does the can buckle? Assume the yield strength is 180 MPa and the elastic modulus is 69 GPa. A= 1= rg= The slenderness ratio is: 0J = x10^-9 m^4 The slenderness ratio is: Johnson equation )/( x10^-5 m^2 The buckling load P= m The buckling load An MPa N ) =arrow_forwardRigid bar ABC is supported by bronze rod (1) and aluminum rod (2), as shown. A concentrated load P is applied to the free end of aluminum rod (3). Bronze rod (1) has an elastic modulus of E₁ = 15,000 ksi and a diameter of d₁ = 0.40 in. Aluminum rod (2) has an elastic modulus of E₂ = 10,000 ksi and a diameter of d₂ = 0.70in. Aluminum rod (3) has a diameter of d3 = 1.00in. The yield strength of the bronze is 48 ksi and the yield strength of the aluminum is 40 ksi. Assume a = 2.5 ft, b = 1.5 ft, L₁= 6 ft, L₂= 8 ft, and L3 = 3 ft. (a) Determine the magnitude of load P that can safely be applied to the structure if a minimum factor of safety of 1.8 is required. (b) Determine the deflection of point D for the load determined in part (a). (c) The pin used at B has an ultimate shear strength of 57 ksi. If a factor of safety of 2.7 is required for this double shear pin connection, determine the minimum pin diameter that can be used at B. L₁ T A Bronze (1) B Aluminum (3) D Aluminum P b (2) L3 •…arrow_forward
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