H.W 3 Two aluminum alloyplates (2) are attached to thesides of a wooden beam (1) asshown in Figure 3.mensions of the composite crosssection are b = 80 mm, di240 mm, b2 = 10 mm, d2b2b2The di-d2di%3D120 mm, and a = 60 mm. Deter-(2)|(2)(1)mine the maximum bendingstresses produced in both thewooden beam and the aluminumaplates if a bending momentM = +6,000 N.m is appliedabout the z axis. Assume that Ej =12.5 GPa and E2 = 70 GPa.FIGURE 3

Answered: Image /qna-images/answer/03aae36d-21e7-4400-b4d1-cdda8578a0d6.jpg

H.W 3_ Two aluminum alloy plates (2) are attached to the sides of a wooden beam (1) as shown in Figure 3. mensions of the composite cross section are b = 80 mm, d 240 mm, b2 = 10 mm, d2 120 mm, and a = 60 mm. Deter- b2 The di- d2 di %3D %3D (2) |(2) mine the maximum bending stresses produced in both the (1) wooden beam and the aluminum plates if a bending moment M = +6,000 N · m is applied about the z axis. Assume that Ej = 12.5 GPa and E2 = 70 GPa. FIGURE 3 %3D

H.W 3_ Two aluminum alloy plates (2) are attached to the sides of a wooden beam (1) as shown in Figure 3. mensions of the composite cross section are b = 80 mm, d 240 mm, b2 = 10 mm, d2 120 mm, and a = 60 mm. Deter- b2 The di- d2 di %3D %3D (2) |(2) mine the maximum bending stresses produced in both the (1) wooden beam and the aluminum plates if a bending moment M = +6,000 N · m is applied about the z axis. Assume that Ej = 12.5 GPa and E2 = 70 GPa. FIGURE 3 %3D

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

See similar textbooks

Similar questions

A composite beam is made of two brass [E =101 GPa] plates bonded to an aluminum [E =64 GPa] bar, as shown in Figure below. The beam is subjected to a bending moment of 2030 N-m acting about the z axis. Assume b=53 mm, d1=52 mm, d2 =11 mm, Determine: (a)the maximum bending stresses in the brass plates and the aluminum bar. (b) the stress in the brass at the joints where the two materials are bonded together.
i need the answer quickly
For the beam shown in figure: 1. Compute maximum tensile stress and compressive stress devloped in the beam 2. Determine the type and magnitude of the flexural stress in a fiber located at y1 = 25mm , from the bottom for a section 6m from the left end of the beam
2. In a laboratory test of a beam loaded by end couples, the fibers at layer AB in Figure below are found to increase 60 x 10-3 mm whereas those at CD decrease 100 x 103 mm in the 200-mm-gage length. Using E=70 GPa, determine the flexural stress in the top and bottom fibers. 200 mm 30 mm B 120 mm 30 mm Hello sir, please solve detailed details, boring, new article, I didn't understand anything, please sir, thank you sir. A how detailed solution
AC D BC BD C Figure of Question 2 Beam AC is subjected to a uniformly distributed load of w= 4.8 kN/m. The beam, which has a moment of inertia of 246(106) mm¹, is fixed at A and supported by rod BD. The rod BD is pinned at both of its ends, and has a cross-sectional area of 24 mm². Both beam AC and rod BD has a Young's modulus of 216 GPa. Given lengths AC = 4.0 m, BC = 1.0 m, and BD = 1.5 m. Find the vertical displacement at point C due to the distributed load w
Only do equivalent to steel
first two number my student number= 17
Shown below is a rigid beam ABC that is connected by pinned connections to rod (1) at A, rod (2) at C, and pivots freely at B. Rod (1) is made of bronze (E=100GPA, a=16.9x10-6/°C) and is 24mm in diameter. Rod (2) is made of aluminum (E=70GPA, a=22.5x10-6/°C) and is 16mm in diameter. The bars are unstressed as shown at 25°C. The temperature of bar (2) is reduced to 10°C while the temperature of bar (1) is held constant. Find the normal stress in bars (1) and (2). 250mm (1) |이 B A 200mm 350mm 500mm (2)