A bronze pipe (1) is to be connected to analuminum alloy pipe (2) at flange B. When put in place, however, a gap of A - 0.20 in. existsbetween the two pipes. Bronze pipe (1) has an elastic modulus of E, - 16,000 ksi, a cross-sectional area of Az - 2.75 in.?, and a lengthof L1- 44 ft. Aluminum alloy pipe (2) has an elastic modulus of E2 - 10,000 ksi, a cross-sectional area of A2 - 1.32 in. 2, and a length ofL2 - 10.5 ft. If bolts are inserted in the flanges and tightened so that the gap at Bis closed, determine:(a) the normal stresses produced in each of the members.(b) the final position of flange B with respect to support A.L2В(2)(1)Answer:(2) 01-ksi02 -ksi(b) OB/A -in.

Answered: Image /qna-images/answer/8577722e-ac7e-4630-a13d-87c84973058a.jpg

A bronze pipe (1) is to be connected to an aluminum alloy pipe (2) at flange B. When put in place, however, a gap of A - 0.20 in. exists between the two pipes. Bronze pipe (1) has an elastic modulus of E, - 16,000 ksi, a cross-sectional area of A, - 2.75 in.?, and a length of L, - 4.4 ft. Aluminum alloy pipe (2) has an elastic modulus of Ez - 10,000 ksi, a cross-sectional area of A2 - 1.32 in. 2, and a length of L2 - 10.5 ft. If bolts are inserted in the flanges and tightened so that the gap at Bis closed, determine: (a) the normal stresses produced in each of the members. (b) the final position of flange B with respect to support A. L2 B cl Answer: (a) 0z - ksi 02- ksi (b) ðe/a - in.

A bronze pipe (1) is to be connected to an aluminum alloy pipe (2) at flange B. When put in place, however, a gap of A - 0.20 in. exists between the two pipes. Bronze pipe (1) has an elastic modulus of E, - 16,000 ksi, a cross-sectional area of A, - 2.75 in.?, and a length of L, - 4.4 ft. Aluminum alloy pipe (2) has an elastic modulus of Ez - 10,000 ksi, a cross-sectional area of A2 - 1.32 in. 2, and a length of L2 - 10.5 ft. If bolts are inserted in the flanges and tightened so that the gap at Bis closed, determine: (a) the normal stresses produced in each of the members. (b) the final position of flange B with respect to support A. L2 B cl Answer: (a) 0z - ksi 02- ksi (b) ðe/a - in.

Structural Analysis

6th Edition

ISBN:9781337630931

Author:KASSIMALI, Aslam.

Publisher:KASSIMALI, Aslam.

Chapter2: Loads On Structures

Section: Chapter Questions

Problem 1P

See similar textbooks

Similar questions

The double T-beam is fabricated by welding the three plates together as shown. Part A Determine the shear stress in the weld necessary to support a shear force of V=78 kN�=78 kN.
An aluminum alloy [E = 10,000 ksi; σY = 40 ksi] pipe (1) is connected to a bronze [E = 16,000 ksi; σY = 45 ksi] pipe at flange B. The pipes are attached to rigid supports at A and C. Pipe (1) has an outside diameter of 2.100 in., a wall thickness of 0.21 in., and a length of L1 = 7 ft. Pipe (2) has an outside diameter of 5.00 in., a wall thickness of 0.23 in., and a length of L2 = 12 ft. If a minimum factor of safety of 1.4 is required for each pipe, determine:(a) the maximum load P that may be applied at flange B.(b) the deflection of flange B at the load determined in part (a). Deflection to the right is positive.
Solv it ,thanks.
The axial assembly consists of a solid 1.01-in.-diameter aluminum alloy [E = 9000 ksi, v = 0.32, a = 13× 10-6/°F] rod (1) and a solid 1.4-in.-diameter bronze [E = 15600 ksi, v = 0.17,a = 9× 10-6/°F] rod (2). ASsume L1=15 in., L2=23 in. If the supports at A and C are rigid and the assembly is stress free at 8°F, determine: (a) the normal stresses o1,02 in both rods at 177°F (positive if tensile, negative if compressive). (b) the displacement ug of flange B (positive if to the right, negative to the left). (c) the change in diameter Ad¡ of the aluminum rod. B C (1) (2) L1 L2 Answers: ( a) σ1 i ksi, o2 = i ksi (b) UB = i in. (c) Adı = in. i
Current Attempt in Progress X Incorrect Compound axial member ABC has a uniform diameter of d- 1.25 in. • Segment (1) is an aluminum [Ez - 10000 ksi]alloy. The length of segment (1) is L4 - 70 in. • Segment (2) is a copper [E2 - 17000 ksi]alloy. The length of segment (2) is L2 - 98 in. When axial force Pis applied, a strain gage attached to copper segment (2) measures a normal strain of 2 - 2100 uin./in. in the longitudinal direction. What is the total elongation of member ABC? L2 Aluminum B Соpper Answer: AL - 35.7 in.
7. ASTM suggests a tolerance of... percent to allow the variation in strength as a test of ....w. water. A. 12 В. 8 C. 10 D. 15 E. 16 F. None of them
dont round off if not yet the final answer pls
please help me to design a simple tensile structure for the exhibition space roof
An aluminum alloy [E = 10,000 ksi; σY = 40 ksi] pipe (1) is connected to a bronze [E = 16,000 ksi; σY = 45 ksi] pipe at flange B. The pipes are attached to rigid supports at A and C. Pipe (1) has an outside diameter of 2.150 in., a wall thickness of 0.16 in., and a length of L1 = 6 ft. Pipe (2) has an outside diameter of 5.10 in., a wall thickness of 0.19 in., and a length of L2 = 10 ft. If a minimum factor of safety of 1.6 is required for each pipe, determine:(a) the maximum load P that may be applied at flange B.(b) the deflection of flange B at the load determined in part (a). Deflection to the right is positive.
A 2014-T6 aluminum tube having a cross-sectional area of 600 mm² is used as a sleeve for an A-36 steel bolt having a cross-sectional area of 400 mm², When the temperature is T=15 °C, the nut holds the assembly in a snug position such that the axial force in the bolt is negligible. If the temperature increases to T-80 °C and an axial force of 25 KN is applied to the assembly, determine the stresses in the bolt and the sleeve. Note: Length of the assembly is 150 mm, E is 200 Gpa, a is 12*106 (for bolt), E is 73.1 Gpa, a is 23*106 (for sleeve).
The given plate below with width of 200 mm andthickness of 16 mm is to be connected to two plates ofthe same width with half the thickness by 20 mmdiameter rivets as shown. The rivet hole is 2 mm greaterthan the rivet diameter. Allowable tensile stress on netarea is 0.6Fy. Allowable bearing stress is 1.35Fy. plate: fy = 241 mpa fu = 4141 mpa rivet: fv = 152 mpa a. Determine maximum load P without exceeding allowable tensile stress on plate b. Determine maximum load P without exceeding allowable shear stress on rivets c. Determine maximum load P without exceeding allowable bearing stress between plates and rivets
Steel