shear strain at point A relative to x-y axis
shear strain = tan-1(18/(163+13))
shear strain = 0.1023 rad
so,option 3 is correct , 0.1023.
Considering the figure shown, the shear strain at point A relative to the x-y axes is:...
Considering the figure shown, the shear strain at point A relative to the x-y axes is: у -16 418/ B' CH B С 13 163 A D х 44
Question 7 Considering the figure shown, the shear strain at point A relative to the x-yaxes is: 5 mm y 0.4 m 3 mm 0.3 m А 0.964 0 -0.964 0.0168 0.0168 MacBook Air 80 GOS 000 F FS 97 # $ A 3 4 % 5 * ON & 7 8 9
Considering the figure shown, the normal strain on side A-B is: 116 +187 B' C' B С 13 163 А D х x 44- -0.085 0.085 0.075 -0.075
Question 7 Considering the figure shown, the shear strain at point A relative to the x-yaxes is: 5 mm у 0.4 m 3 mm 0.3 m А 0.964 0 -0.964 0.0168 -0.0168 MacBook Air 80 GOS 000 F4 FS 97 # $ 4 A 3 % 5 & ON 7 8
Part A: Average normal strain along AC Determine the average normal strain (ϵAC)avg along AC after the load has been applied. Part B: Average shear strain at A Determine the average shear strain γxy at A relative to the x and y axes. Part C: Average shear strain at point C Determine the average shear strain γxy at point C relative to the x and y axes after deformation. Learning Goal: To determine the average normal strain and average shear...
The square deforms into the position shown by the dashed lines. (Figure 1) The dimensions are S 49 mm, S,-54 mm, ΔΧ1-4 mm, and ΔΖ2 : 8 mm. Side D'B, remains horizontal Part A Determine the shear strain at A relative to the z, y axes. Express your answer to three significant figures and include appropriate units Tay262-102 rad Previous A nswe Figure 1 of 1 Correct Ar Part B Determine the shear strain at B relative to the z,...
The rectangular plate deforms as shown by the dashed lines. Determine the shear strain ?xy at Point A. Determine the shear strain ??′y′ atPointA. T 0.01 in 5 in X 0.02 in.- ---0.02 in -5 in. A -5 in
strain rosette shown in the figure was used to obtain normal strain data at a point on the free surface of a machine component. E-220 GPa, va0.3, a,--1 25 με, 6-95 μ, e-310 μα] Determine the shear stress in the xy plane. 71.1 MPa -89.7 MPa 41.8 MPa 97.1 MPa -33.3 MPa strain rosette shown in the figure was used to obtain normal strain data at a point on the free surface of a machine component. E-220 GPa, va0.3, a,--1...
1. The nonzero stress components relative to axes (x, y, z) are Oxx = -90 MPa, Oyy = 50 MPa, and Oxy= 6 MPa. a. Determine the principal stresses, 01202203 b. Calculate the maximum shear stress. c. Calculate the octahedral shear stress. d. Determine the angle between the x axis and the X axis, where X is in the direction of the principal stress 01.
The square detorms into the position shown by the dashed lines. (Figure 1) The dirmensions are S56mm, s' = 59 mm, Δ#1 = 4 mm, and Δ*2 = 6 mm. Side D 'B'remains horizantal. (vi),,--0.221 rad Submit X Incorrect; Try Again; One attempt remaining Part C Determine the shear strain at C relative to the z, y axes. Figure 1 of 1 Express your anser to three significant figures and include appropriate units. As y0.2062 rad 91.5 Submit Previous Answers...