Evaluating
along all three rosettes
individually starting from first rosette using standard equation of
Mohr's Circle
1=
+
+
-Eq (1)
2=
+
+
Now expanding
and
using cos and sin identities
We get;
2=
+
+
Putting values of sin and cosine we get;
2=
+
+
- Eq (2)
And Now for
3 we get;
3=
+
+
Now expanding
and
using cos and sin identities
We get;
3=
+
+
Putting values of sin and cosine we get;
3=
+
+
- Eq(3)
Now adding Eq(1), Eq(2), Eq (3)
We get:
1+
2+
3=
+0+0
and as
=
avg
We get;
1+
2+
3=
avg
For a 60 degree strain rosette shown in the figure, prove that the sum of the...
please provide a neat, correct and order wise solution thanks,
thumbs up
On the aluminum plate (E-70GPa, v= 0.25), three 45° rosette gages measure E4-5001, a.-150μ and 2001, respectively (,-"X 10-6"). Note the alignments of the gages with respect to the coordinate axes as shown. 45° (a) Determine the strain components a, a, & and (b) Compute the stress components o, σ , o, and Tp, using the Hooke's law, and the strain energy density JH (c) (extra credit 4pts)...
1) An element in plane strain has a 60° strain rosette that is 150 from the x axis. Use Mohr's circle to determine. E = 29,000 ksi G= 11,200 ksi &=-.0015 E, = .004 E = -0025 a) The principal strains and maximum shear strain. b) Determine the location of the principal strains. c) Determine the stresses from the strains given d) Determine the stresses from the principal strains
Question 4 - (25 marks) 4a) The 60° strain rosette, shown in Figure 6, -is mounted on a beam. The following readings are obtained from each gauge: Ea= 250 u ; Eb= -400 u ; Ec= 280 u Determine:- (9) i. The in-plane principal strains and their orientation, and ii. The maximum in-plane shear strain and the average normal strain. of the principal plane. (6) b a 60° 60° 60°
18 pts total 10.3-4. A 60-degree rosette has the given strain gauge measurement values. Determine a,b,c) normal strains in x & y directions and xy-shear strain, d) average normal strain, e) maximum physical shear strain (not the radius in Mohr's circle), and f) maximum principal strain. You entered/3pts > = Normal strain in X-direction & (LL inlin) You entered/3 pts > = Normal strain in Y-direction &y (L inlin) J'ou entered/3pts > = Shear strain in XY-plane Yay (L inlin)...
A strain rosette with as shown, the measured strains
are . Determine the shear stress if
E = 70 GPa and v = 0.25
1 = 0º, e2 = 45°, 03 = 135° {1 = 300 um/m, &z = 100 um/m, 3 = 10 um/m. {2 3 E2 өз 1 м 3 ө х о
For a strain rosette with @1 = 0°, 02 = 45°, 03 = 135° as shown, the measured strains are € 1 = 300 um/m, £2 = 100 um/m, 3 = 10 um/m. Determine the shear stress if E = 70 GPa and D = 0.25.Enter your answer in MPa up to the first decimal place 1 www.ameswab.info
its 45 deg rosette.Not 60 degree
Problem 1: The 60 deg strain rosette is mounted on a steel plate (E = 30e6 psi, G = 11.5e6 psi). Readings obtained from each gage are shown below. Using strain transformation equations, determine Ex, Ey and Yxy. Solve for Ox, Oy and Txy. Draw the stress element with values and directions. €2 = 737e-6 £1 = 389e-6 45° 45° £3 = -290e-6
Create stress mohr circle based on these values and determine
principal stress and maximum shear stress. Also describe the
loading condition that produced these data. Determine the strain is
present if stressx= 100MPa, stressy= -50MPa, stressxy= 30MPa.
Assume aluminum alloy
Hooke's Law The free-surface of a structure is in plane stress if gravity and other body forces are neglected. Because there are 3 unknowns (σ, oy, t»), 3 measurements are generally required in order to determine the stress or strain...
Part A - Question 3 (Total Marks for Part A - Question 3:20) A steel beam in an industrial structure is part of a complicated frame that was difficult to analyse. Using a rectangular strain gauge rosette, the actual strains at point A have been recorded while being subjected to test loads. It is necessary to determine the normal stresses and shear stresses in the actual beam subject to the test loads to check whether the stresses assumed in the...
Question 1 The cylindrical pressure vessel shown has an inside diameter of 625 mm and a wall thickness of 5 mm. The cylinder is made of an aluminum alloy that has an elastic modulus of E = 70 GPa and a shear modulus of G-26.3 GPa. Two strain gages are mounted on the exterior surface of the cylinder at right angles to each other; however, the angle θ is not known. If the strains measured by the two gages are...