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The stress-strain diagram for a steel alloy, which the plates in the figure 1 are made of, is given in the figure 2. Determine: V NL 1.The maximum normal stress developed in the structure. 2. Shear stress developed in the structure. 3. Total displacement of point A with respect to the support. Gavg = A Tavg o = Ee 8 = E- EA A

The stress-strain diagram for a steel alloy, which the plates in the figure 1 are made of, is given in the figure 2. Determine: V NL 1.The maximum normal stress developed in the structure. 2. Shear stress developed in the structure. 3. Total displacement of point A with respect to the support. Gavg = A Tavg o = Ee 8 = E- EA A

Elements Of Electromagnetics
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
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Ignore bolt hole for pt 3

The stress-strain diagram for a steel alloy, which the plates in the figure 1 are made of, is given in the figure 2. Determine: 1.The maximum normal stress developed in the structure. 2. Shear stress developed in the structure. 3. Total displacement of point A with respect to the support. N Gavg V Tavg a = Ee 8 = E EA NL A a (ksi) .-61 60 40 in. (Typ.) 50 -47. 20 in. (Typ.) (ay) - 38.40 (oy) - 36 3530 20 900kips 10 2 in. (Typ.) 0.050 0.1o ey-0030 e (in./in.) 0.20 0.002 Et-0.0012 0.30 0,40 0.001 0.003 0.004 1.50 in. Stress-strain diagram for mild steel Figure 1. Figure 2.
Transcribed Image Text:The stress-strain diagram for a steel alloy, which the plates in the figure 1 are made of, is given in the figure 2. Determine: 1.The maximum normal stress developed in the structure. 2. Shear stress developed in the structure. 3. Total displacement of point A with respect to the support. N Gavg V Tavg a = Ee 8 = E EA NL A a (ksi) .-61 60 40 in. (Typ.) 50 -47. 20 in. (Typ.) (ay) - 38.40 (oy) - 36 3530 20 900kips 10 2 in. (Typ.) 0.050 0.1o ey-0030 e (in./in.) 0.20 0.002 Et-0.0012 0.30 0,40 0.001 0.003 0.004 1.50 in. Stress-strain diagram for mild steel Figure 1. Figure 2.
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