Steel Design (Activate Learning with these NEW titles from Engineering!)
6th Edition
ISBN: 9781337094740
Author: Segui, William T.
Publisher: Cengage Learning
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Chapter 9, Problem 9.1.6P
To determine
The nominal flexural strength of the composite beam given in problem 9.1-3.
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A composite bar BCD has a uniform external radius R, = 9cm. Segment BC is solid steel, while segment CD is
composed of a copper core of radius R= 1cm bonded inside a steel sleeve. The lengths of the two segments are
LEc= 2 m and Leo= 1 m. The material moduli are Ege= 200 GPa and E- 100 GPa. The bar is fixed at B and
tensile loads are applied at section D (F»= 1000 kN) and at section C (Fc= 400 kN). Compute the following:
What is the Axial stress of steel in segment BC in MPa?
2m
B
1m
D
400 KN
1000 KN
Chapter 9 Solutions
Steel Design (Activate Learning with these NEW titles from Engineering!)
Ch. 9 - Prob. 9.1.1PCh. 9 - Prob. 9.1.2PCh. 9 - Prob. 9.1.3PCh. 9 - Prob. 9.1.4PCh. 9 - Prob. 9.1.5PCh. 9 - Prob. 9.1.6PCh. 9 - A W1422 acts compositely with a 4-inch-thick floor...Ch. 9 - Prob. 9.2.2PCh. 9 - Prob. 9.3.1PCh. 9 - Prob. 9.3.2P
Ch. 9 - Prob. 9.4.1PCh. 9 - Prob. 9.4.2PCh. 9 - Prob. 9.4.3PCh. 9 - Prob. 9.4.4PCh. 9 - Prob. 9.4.5PCh. 9 - Prob. 9.5.1PCh. 9 - Prob. 9.5.2PCh. 9 - Prob. 9.5.3PCh. 9 - Note For Problems 9.6-1 through 9.6-5, use the...Ch. 9 - Note For Problems 9.6-1 through 9.6-5, use the...Ch. 9 - Note For Problems 9.6-1 through 9.6-5, use the...Ch. 9 - Note For Problems 9.6-1 through 9.6-5, use the...Ch. 9 - Note For Problems 9.6-1 through 9.6-5, use the...Ch. 9 - Prob. 9.7.1PCh. 9 - Prob. 9.7.2PCh. 9 - Prob. 9.7.3PCh. 9 - Prob. 9.7.4PCh. 9 - Prob. 9.8.1PCh. 9 - Prob. 9.8.2PCh. 9 - A beam must be designed to the following...Ch. 9 - Prob. 9.8.4PCh. 9 - Prob. 9.8.5PCh. 9 - Prob. 9.8.6PCh. 9 - Prob. 9.8.7PCh. 9 - Prob. 9.8.8PCh. 9 - Use the composite beam tables and select a W-shape...Ch. 9 - Prob. 9.8.10PCh. 9 - Prob. 9.10.1PCh. 9 - Prob. 9.10.2P
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- View Policies Current Attempt in Progress A composite beam is made of two brass [E-94 GPa] plates bonded to an aluminum [E-70 GPa] bar, as shown. The beam is subjected to a bending moment of 1850 N-m acting about the z axis. Assume b-57 mm, d₁-43 mm, d₂-9 mm. Determine: (a) the maximum bending stresses Obr. Gal in the brass plates and the aluminum bar. (b) the stress in the brass brj at the joints where the two materials are bonded together. 2 Brass (2) Aluminum (1) Brass (2) Answers: (a) abr = (b) Obrj = i i b MPa, Gal = i MPa. MPa.arrow_forwardA composite section consisting of copper and steel carries an axial compressive force P. Both the materials have equal lengths. For steel, A_st=900 [mm] ^2,E_st=200 GPa,o (allowable,st)=140 MPa. For copper, A_cu=1200 [mm] ^2,E_cu=120 GPa,0_(allowable,cu)=70 MPa. Determine the maximum load (kN) the member can carry so that an allowable strain of 0.0005 is not exceeded. A) 210 kN B 105 kN 162 kN D 189 kNarrow_forwardhelp me asaparrow_forward
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- Problem 2. A W12×58 acts compositely with a 5-inch-thick concrete slab. The effective slab width is 70 inches. Shoring is not used, and the applied bending moments are as follows: From the beam weight, Mbeam= 15 ft-kips From the slab weight, Malab = 80 ft-kips From the live load, ML = 150 ft-kips Do not consider the construction loads. Steel A992, and f. = 4 ksi. Determine whether the flexural strength of this beam is adequate. Assume full composite action and assume that the formwork provides lateral support of the steel section before curing of the concrete. Assume that W12x58 is a compact section.arrow_forwardComposite beams Probelm.arrow_forwarddetermine the moment of inertia of the composite area about x and y axis. a=3 b=6 c=3 d=4arrow_forward
- Q3\ The composite bar is firmly attached to unyielding supports. Compute the stress in each material caused by the application of the axial load P = 40 kips. %3D Steel Aluminum A = 1.25 in.2 E = 10 x 106 psi A = 2.0 in.2 E = 29 x 10° psi P to 12 in. 15 in-arrow_forwardThe composite bar shown is firmly attached to unyielding supports. An axial load P- 269 kN is applied at 28 °C. Find the stress in the aluminum at 68 C. Assume a= 11.7 um/(mC) for steel and 23 um/{mC) for aluminum. Given: Ea =70 GPa, Aa - 968 mm, La - 228 mm, Es = 211 GPa, As=1,265 mm, Ls= 374 mm, Answer must be in MPa. Aluminum Steel La Lsarrow_forwardComposite beam as shown. If allowable normal stress for steel is (ollow)st = 168 MPa and for wood is (Callow)w = 21 MPa, determine maximum bending moment beam can support, with and without reinforcement. E = 200 GPa, E= 12 GPa, st W Moment of inertia of steel beam is I, = 7.93 × 106 mmª, X-sectional area is A = 5493.75 mm² 100 mm, 5 mm 105 mm 30 mm (a)arrow_forward
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