Determine the maximum compressive and tensile stress of the section

Q: AN ALUMINUM TUBE IS FASTENED BETWEEN A STEEL ROD AND BRONZE ROD AS SHOWN IN THE FIGURE. AXIAL LOADS…

A: Es = 210GPa  EAl = 65GPa  EB = 80GPa

Q: 10 MPа 4 ksi 10 MPа 4 ksi 10 MPа 2 ksi

A: Solution:- 1. Radius of Mohr's circle: r=σx-σy22+τxy2  =10-1002+0  =0 2. Radius of Mohr's circle:…

Q: The normal and shear stresses acting on element A are 6,650 psi, 17,600 psi, and 2,700 psi (see part…

A:

Q: Determine bending stress formula

A: To find bending stress formula

Q: small aluminum alloy [E = 65 GPa] tee shape is used as a simply supported beam as shown. For this…

A: Calculating the reactions:

Q: A mild steel bar, 1.5 m long, has a square section 40 mm x 40 mm. The bar is subjected to a two-…

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Q: A mild steel bar, 1.5 m long, has a square section 40 mm x 40 mm. The bar is subjected to a two-…

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Q: ЗР Strain gage 1.1, a a H Answer: P = i 369 N

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Q: Determine the normal and shear stresses that occur in the n-n plane of the figure. Present a diagram…

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Q: A small aluminum alloy [E = 62 GPa] tee shape is used as a simply supported beam as shown. For this…

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Q: A small aluminum alloy [E = 62 GPa] tee shape is used as a simply supported beam as shown. For this…

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Q: Asmall aluminum alloy [E = 74 GPa] tee shape is used as a simply supported beam as shown. For this…

A:

Q: what differ between plane stress and strain.As like pancel is which of those? （eg,a pancil ,glass…

A: Given data: Difference between Plane stress and Plane strain.

Q: A small aluminum alloy [E = 71 GPa] tee shape is used as a simply supported beam as shown. For this…

A:

Q: A small aluminum alloy [E = 79 GPa] tee shape is used as a simply supported beam as shown. For this…

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Q: small aluminum alloy [E = 74 GPa] tee shape is used as a simply supported beam as shown. For this…

A:

Q: Determine the maximum tensile stress in the loaded beam shown.

A: Maximum moment is at Support BMMax=-505m=-250kN-m hogging

Q: Find the Stress if Tensile force 2.3 N applied on rod having cross sectional area of 1 mm2

A: Introduction : The question is related with solid mechanics . In this question the data of tensile…

Q: Answer: P = %3D Save for Later Using multiple attempts will impact your score. 5% score reduction…

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Q: A small aluminum alloy [E = 65 GPa] tee shape is used as a simply supported beam as shown. For this…

A: Given,  There is a simply supported beam.  Our aim is to determine the Load (P) value.    So let's…

Q: A small aluminum alloy [E = 61 GPa] tee shape is used as a simply supported beam as shown. For this…

A:

Q: A small aluminum alloy [E = 76 GPa] tee shape is used as a simply supported beam as shown. For this…

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Q: P ЗР Strain gage- d 1.1,1,P.. E H

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Q: A small aluminum alloy [E = 65 GPa] tee shape is used as a simply supported beam as shown. For this…

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Q: The rectangular steel plate in the figure is forced by the forces given at the A and B points. a)…

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Q: What is the applied load P

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Q: The truss is made from three pin-connected members having the cross-sectional areas shown in the…

A: Given

Q: Jor 6 m 5 kN/m -250 mm 20 mm-

A: Determine the maximum tensile stress in the following beam:

Q: A small aluminum alloy [E = 80 GPa] tee shape is used as a simply supported beam as shown. For this…

A:

Q: A small aluminum alloy [E=77 GPa] tee shape is used as a simply supported beam as shown. For this…

A: Given Data: E=77 Gpa a=160mm b=22mm c=10mm d=33mm t=4mm Normal strain=410   It is asked to…

Q: 2. (3 points) When loading is applied at a point on a body, the stress distributions at different…

A: Saint Venant’s principle

Q: 6 kN A B C 120 40 -90- Dimensions in mm 40 1m 1.2m 2 kN

A:

Matrix Algebra for Structural analysis

Structural analysis is a process in which the effects of different loads and internal forces, acting on structures and their elements are determined. This method of analysis is effective in detecting the failure loads of the structural elements and the design can be altered before commencing the construction process, which ensures proper strength and safety of the structures.