Steel Design (Activate Learning with these NEW titles from Engineering!)
6th Edition
ISBN: 9781337094740
Author: Segui, William T.
Publisher: Cengage Learning
expand_more
expand_more
format_list_bulleted
Question
Chapter 6, Problem 6.8.2P
To determine
The lightest
Expert Solution & Answer
Want to see the full answer?
Check out a sample textbook solutionStudents have asked these similar questions
The two span beam shown in the figure has L1 = L2 = 5.0 m. The service loads are total dead load of 5.4 kN/m and live load of 8.7 kN/m. If live load is placed to produce maximum positive moment on span AB, calculate the maximum factored positive bending moment at span AB in kN-m. Write your answer in 2 decimal places only without the unit.
F=16 kN single load, M=22 kN.m moment and w=4 kN/m distributed load are acting on the beam whose loading condition is given in the figure. The length L is also given as L=2 m. The cross-sectional properties of the beam are; body height yg=244 mm, body thickness xg=10 mm, flange width xf=173 mm, flange height yf=18 mm. Point E on the section is located just below the flange-body junction. It is desired to determine the stress state in the section taken from the B level of the beam. According to this;
Question1-A) Find the support response (Dy) at point D. (Write your result in kN.)
Question1-B) Find the support response (Ay) at point A. (Write your result in kN.)
Question1-C) Find the shear force (VB) at point B. (Write your result in kN.)
Question1-D) Find the bending moment (MB) at point B. (Write your result in kN.m.)
Question 1-E) Find the y distance of the center of the section with respect to the axis passing through the base of the section (Write your result in mm.)
Question 1-F)…
F=16 kN single load, M=22 kN.m moment and w=4 kN/m distributed load are acting on the beam whose loading condition is given in the figure. The length L is also given as L=2 m. The cross-sectional properties of the beam are; body height yg=244 mm, body thickness xg=10 mm, flange width xf=173 mm, flange height yf=18 mm. Point E on the section is located just below the flange-body junction. It is desired to determine the stress state in the section taken from the B level of the beam. According to this;
Question1-A) Find the support response (Dy) at point D. (Write your result in kN.)
Question1-B) Find the support response (Ay) at point A. (Write your result in kN.)
Question1-C) Find the shear force (VB) at point B. (Write your result in kN.)
Question1-D) Find the bending moment (MB) at point B. (Write your result in kN.m.
Chapter 6 Solutions
Steel Design (Activate Learning with these NEW titles from Engineering!)
Ch. 6 - Prob. 6.2.1PCh. 6 - Prob. 6.2.2PCh. 6 - Prob. 6.6.1PCh. 6 - Prob. 6.6.2PCh. 6 - Prob. 6.6.3PCh. 6 - The member shown in Figure P6.6-4 is part of a...Ch. 6 - Prob. 6.6.5PCh. 6 - Prob. 6.6.6PCh. 6 - Prob. 6.6.7PCh. 6 - Prob. 6.6.8P
Ch. 6 - Prob. 6.6.9PCh. 6 - Prob. 6.6.10PCh. 6 - Prob. 6.6.11PCh. 6 - Prob. 6.6.12PCh. 6 - Prob. 6.6.13PCh. 6 - Prob. 6.7.1PCh. 6 - Prob. 6.7.2PCh. 6 - Prob. 6.8.1PCh. 6 - Prob. 6.8.2PCh. 6 - Prob. 6.8.3PCh. 6 - Prob. 6.8.4PCh. 6 - Prob. 6.8.5PCh. 6 - Prob. 6.8.6PCh. 6 - Prob. 6.8.7PCh. 6 - Prob. 6.8.8PCh. 6 - Prob. 6.8.9PCh. 6 - Prob. 6.8.10PCh. 6 - Prob. 6.9.1PCh. 6 - Prob. 6.9.2P
Knowledge Booster
Similar questions
- A compression member s built up from a W14 x 90 and a W10 x 49, both of A992 steel with Fy = 50 ksi and E = 29000 ksi. Determine the moment of Inertia along the centroidal x-axis of this built up section,in in^4.arrow_forwardDesign the lightest W shape beam of 50 ksi steel to support the loads shown in the figure. Neglect the beam self-weight. The beam has continuous lateral bracing between A and B, but is laterally unbraced between B and C. Determine Cb.arrow_forwardA wide-flange section is used as a beam. The properties of the W-section are:bf = 135 mm,tf = 25 mm,bw = 30 mm,d = 450mm,E = 50 MPa.The beam is subjected to a uniformly distributedload as shown, where W = 20 N/m.Find the: value of P so that thedeflection at point C is zero, the value of P so that thedeflection at C is 150/EI downward, the value of P so that thedeflection at point C is 150/EI upward.arrow_forward
- 'The I-beam is loaded as shown in the figure. Determine the required flange width b so that the stress caused by bending does not exceed the allowable stress σmax = 170 MPa. The thickness of the flange is tflange= 12 mm, and the thickness of the web inch tweb= 8 mm, so let's look at just bending. F = 48kN, q = 8kN/m, L = 2.2m, H = 500mm Use units [N, mm]. Enter the answer to one decimal place. Do not round the invoices in the intermediate stages, but only the final answer!arrow_forwardThe rigid beam embedded in the Figure is fixed at the top by two posts, one in AISI 4340 steel (dext = 40mm) and the other in 6063-T6 aluminum. If it is desired that the beam appears horizontal after applying a homogeneously distributed load of 400 kN/m; Determine the diameter of the aluminum pole that felt this condition. The posts are 500 mm long when no load is applied to the beam. Calculate the longitudinal displacements (δAl , and δFe) and the half stresses (σAl , and σFe) in the posts. Calculate the factors of safety. Use EFe = 200 Gpa , and Eal = 70 Gpa. Elastic limit AISI 4340 (Sy = 786 MPa), and AA6063-T6 (Sy = 214 MPa) (answer :dAl = 67.6 mm δAl = -0.40 mm ; δFe = -0.40 mm σAl = -55.7 Mpa ; σFe = -159 Mpa ; FSAL = 3.8 FSFE = 4.9)arrow_forwardpls answer I'll rate Use virtual work method and determine the following unknowns on the truss system shown below. Use A = 500 mm2 and E = 200 GPa.a. Horizontal displacement of joint G due to the applied loads in mmb. Horizontal displacement of joint G considering that the top chord members experience 60 °C increase in temperature in mm. Use α = 10-6/°Carrow_forward
- F=11 kN single load, M=22 kN.m moment and w=5 kN/m distributed load act on the beam whose loading condition is given in the figure. The length L is also given as L=5 m. The cross-sectional properties of the beam are; body height yg=218 mm, body thickness xg=18 mm, flange width xf=190 mm, flange height yf=13 mm. Point E on the section is located just below the flange-body junction. It is desired to determine the stress state in the section taken from the B level of the beam. According to this;arrow_forwardA.) Draw the shear and moment diagram with label and appropriate values. B.) Find the maximum tensile stress fbtMAX and maximum compressive stress fbcMAX A cantilever beam AB, loaded by a uniform load (see figure), is applied on a channel section. If the cross section has the dimensions indicated and the moment of inertia about the z axis (the neutral axis) is I = 3.36 in4:arrow_forwardA W12x79 of A573 Grade 60 (Fy = 415 MPa) steel is used as a compression member. It is 6.8 m long, fixed at the top and bottom, and has additional support in the weak direction at mid-height. Properties of the section are as follows: A = 14,500 mm^2 Ix = 258.6 x 10^6 mm^4 Iy = 84.375 x 10^6 mm^4 Calculate the critical slenderness ratio with respect to weak axis buckling using theoretical value of k.arrow_forward
- A simply supported beam is loaded as shown. Use E = 200,000MPa and I=150 x 106 mm4. a) Compute for the value of C1 in the equation of the slope for the first segment. b) Compute for the value of C3 (constant of the 1st integration) in the equation of the slope for the 2nd segment.arrow_forwardA W12x79 of A573 Grade 60 (Fy = 415 MPa) steel is used as a compression member. It is 8 m long, pinned at the top fixed at bottom with additional lateral support at mid height in the weak direction. The properties are as follows: Ag = 14,500 sq.mm, Ix= 258.6 x10^6 mm ^4 Iy=84.375 x 10^6 mm^4. 56. Calculate the critical slenderness ratio with buckling about weak axisarrow_forwardA wide-flange beam with an unbalancedcross section has the dimensions shown in the figure.Determine the plastic moment MP if σY = 36 ksi.arrow_forward
arrow_back_ios
SEE MORE QUESTIONS
arrow_forward_ios
Recommended textbooks for you
- Steel Design (Activate Learning with these NEW ti...Civil EngineeringISBN:9781337094740Author:Segui, William T.Publisher:Cengage Learning
Steel Design (Activate Learning with these NEW ti...
Civil Engineering
ISBN:9781337094740
Author:Segui, William T.
Publisher:Cengage Learning