F7-29. The square plate is deformed into the shape shownby the dashed line. Determine the average normal strainalong diagonal AC and the shear strain at point E withrespect to the x and y axes.mm300 mm300 mm -3 тm3 mm

Answered: Image /qna-images/answer/2b4bca2d-3635-4aaf-8ce8-e8ad6125e5d4.jpg

Answered: F7-29. The square plate is deformed…

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

The strain components for a point in a body subjected to plane strain are ɛ, = -460 µe, ɛ, = -990µe and Yy = 219 prad. Using Mohr's circle, determine the principal strains (sp1 > Ep2), the maximum inplane shear strain yip, and the absolute maximum shear strain ymax at the point. Show the angle e, (counterclockwise is positive, clockwise is negative), the principal strain deformations, and the maximum in-plane shear strain distortion in a sketch. Answers: Ep1 = με. Ep2 = με. Yip= prad. Ymax prad.
The strain components at a point in a body subjected to plane strain are E = 850μ, Ey = -300μ, and Yay 400μ. Determine the strain components En, Et, and Ynt at the point if the nt-axes are rotated with respect to the xy-axes as indicate below. = Y t $30% -X n
For the figure shown, if the displacement field is given by {u = axyz}, {v = bxyz} and {w=cxyz} where {a}, {b} and {c} are %3D constants. Determine the normal strain in the {x} direction if the location of point {E*} is (1.506, 1.003,1.991) F F* 2.000 m E D E C 1.500 m B/ 1.000 m Select one: O a. 0.004 b. 0.004 m c. NONE O d. 0.0024 m е. О.0024
The strain components ɛ, Ey, and yy are given for a point in a body subjected to plane strain. Using Mohr's circle, determine the principal strains, the maximum in-plane shear strain, and the absolute maximum shear strain at the point. Show the angle 0, the principal strain deformations, and the maximum in-plane shear strain distortion in a sketch. Ex = 300 µe, ɛ, = -710 pe, Vxy = -440 urad. Enter the angle such that -45°s0,s +45°. Answer: Ep1= pe Ep2= με Ymax in-plane = prad Yabsolute max. prad Əp =
The spherical pressure vessel has an inner diameter of 2 m and a thickness of 10 mm. A strain gage having a length of 20 mm is attached to it, and it is observed to increase in length by 0.012 mm when the vessel is pressurized. Determine the pressure causing this deformation, and find the maximum in-plane shear stress, and the absolute maximum shear stress at a point on theouter surface of the vessel. The material is steel, for which Est = 200 GPa and nst = 0.3.
The rectangular plate is deformed into the shape shown by the dashed lines. Determine the average normal strain along diagonal AC, and the average shear strain at corner A relative to the x, y axes. y 6 mm -400 mm 2 mm 2 mm 300 mm 16 mm 2 mm x A B -400 mm -3 mm
The state of plane strain at a point has strain components of Px = -400(10-6), P y = 200(10-6), and gxy = 150(10-6), Fig. a. Determine the maximum in-plane shear strain and the absolute maximum shear strain.
Determine the deformed length of the elongated diagonal
The strain components ɛx, ɛy, and Yxy are given for a point in a body subjected to plane strain. Using Mohr's circle, determine the principal strains, the maximum in-plane shear strain, and the absolute maximum shear strain at the point. Show the angle 0p, the principal strain deformations, and the maximum in-plane shear strain distortion in a sketch. Ex = 0 µɛ, ɛy = 430 µɛ, Yxy = 230 µrad. Enter the angle such that -45° s 0,s+45°. Answer: Ep1 με Ep2 = Ymax in-plane prad Yabsolute max. prad %3D
*2-4. The force applied at the handle of the rigid lever causes the lever to rotate clockwise about the pin B through an angle of 2°. Determine the average normal strain in each wire. The wires are unstretched when the lever is in the horizontal position. Problem 2-4 A 200 mm 200 mm H C B 300 mm G F 200 mm D 300 mm E
The square plate is such that L = 273 mm. The corners of the square plate are given the displacements di = 7.027 mm and d2 = 4.014 mm. What is the shear strain along the edge of the plate at B? d2 L di di d2
2-11. If a load applied to bar AC causes point A to be displaced to the left by an amount AL, determine the normal strain in wire AB. Originally, 0 = 45°. B L. Probs. 2-10/11

SEE MORE QUESTIONS

Recommended textbooks for you

Elements Of Electromagnetics

Mechanical Engineering

ISBN:

9780190698614

Author:

Sadiku, Matthew N. O.

Publisher:

Oxford University Press

Mechanics of Materials (10th Edition)

Mechanical Engineering

ISBN:

9780134319650

Author:

Russell C. Hibbeler

Publisher:

PEARSON

Thermodynamics: An Engineering Approach

Mechanical Engineering

ISBN:

9781259822674

Author:

Yunus A. Cengel Dr., Michael A. Boles

Publisher:

McGraw-Hill Education

Elements Of Electromagnetics

Mechanical Engineering

ISBN:

9780190698614

Author:

Sadiku, Matthew N. O.

Publisher:

Oxford University Press

Mechanics of Materials (10th Edition)

Mechanical Engineering

ISBN:

9780134319650

Author:

Russell C. Hibbeler

Publisher:

PEARSON

Thermodynamics: An Engineering Approach

Mechanical Engineering

ISBN:

9781259822674

Author:

Yunus A. Cengel Dr., Michael A. Boles

Publisher:

McGraw-Hill Education

Control Systems Engineering

Mechanical Engineering

ISBN:

9781118170519

Author:

Norman S. Nise

Publisher:

WILEY

Mechanics of Materials (MindTap Course List)

Mechanical Engineering

ISBN:

9781337093347

Author:

Barry J. Goodno, James M. Gere

Publisher:

Cengage Learning

Engineering Mechanics: Statics

Mechanical Engineering

ISBN:

9781118807330

Author:

James L. Meriam, L. G. Kraige, J. N. Bolton

Publisher:

WILEY

SEE MORE TEXTBOOKS

F7-29. The square plate is deformed into the shape shown by the dashed line. Determine the average normal strain along diagonal AC and the shear strain at point E with respect to the x and y axes. mm 300 mm 300 mm - 3 тm 3 mm