For the following structures, determine the maximum normal stress,deformation and displacement of point D relative to point A. AlumínioCobreAçoE = 70 GPaEnço = 200 GPaAcD = 39 mm?Ecob= 126 GPaAAB = 58 mm?Anc = 77 mm2%3D16 kN8 kN9 kN7 kNADB16 kN8 kN450 mm+300 mm--400 mm-

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Answered: For the following structures, determine…

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

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In the figure shown, determine the normal stresses at AD and BC + , shearing stress at bolt D bearing stress of AD at bolt D * bearing stress of member EDC at bolt D All bolts Ø16mm 04 im C 0.25 02 m 20kN E 10 x 50 mm 8 x 36 mm
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The state of plane stress at a point is represented by the element shown in the figure. Oy o, = 200 Mpa oy = 450 Mpa Txy Try 3D200 Мра Click here to see all formulas Ox Part A - Determine the maximum principal stress in Mpa. O 253 О 355 O 507 O 760 O 608 Submit Request Answer O O O O O
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The strain rosette shown was used to obtain normal strain data at a point on the free surface of a machine component. Given the values = -165 µμe, e = -155 μe, e = 50 μe, E = 10,600 ksi, and v=0.33, determine (a) the stress components o,,o,, and ry at the point. (b) the principal stresses and the maximum in-plane shear stress at the point; on paper, show these stresses on an appropriate sketch that indicates the orientation of the principal planes and the planes of maximum in-plane shear stress. (c) the magnitude of the absolute maximum shear stress at the point. 45° 45°
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For the following structures, determine the maximum normal stress, deformation and displacement of point D relative to point A.