If the strain or offset is specified as 0.15%, the applied stress plastically deform a 3-inch length to a final length of: a. 3.0015 b. 3.0030 c. 3.0060 d. 3.0045

If the strain or offset is specified as 0.15%, the applied stress plastically deform a 3-inch...
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S. Draw a possible stress strain graph for a material with a yield stress of 300 MPa, an elastic modulus of 200 GPa, a UTS of 450 MPa and a ductility of 20%. Calculate the elastic strain at the point where the material starts to plastically deform. 6. A nylon rope with an elastic modulus of 3 GPa is placed under a force of 17.5 kN. The cross-sectional area of...
Two circular rods are loaded in tension along their longitudinal axis. Both rods have a diameter of 20 mm and a length of 150 mm. One bar is made of aluminum and the other is hot pressed silicon nitride (Si3N4). Both have an applied tensile load of 80 kN. Assume that both materials behave elastically under this loading condition (the aluminum does not plastically deform and the silicon nitride does not fracture) and given the following properties for these materials:EAl= 69 GPa...
Give the following as functions of slug temperature: a. The strain in the slug when d 0.25 inch? (10 pts) b. The strain rate in the slug when d-0.25 inch? (10 pts) c. The flow stress in the slug when d 0.25 inch? (10 pts) d. The pressure in the matrix when d = 0.25 inch? (10 pts) Calculate (algebraically): e. The slug temperature required to keep the force applied by the ram below press capacity? Justify that your force...
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2. Two circular rods are loaded in tension along their longitudinal axis. Both rods have a diameter of 20 mm and a length of 150 mm. One bar is made of aluminum and the other is hot pressed silicon nitride (SigN). Both have an applied tensile load of 80 kN. Assume that both materials behave elastically under this loading condition (the aluminum does not plastically deform and the silicon...
The stress-strain curve for titanium alloy (Ti-6Al-4V) at 427°
C is compared with the stress-strain curves for titanium matrix
composite (TMC) at 25° and 427° C.
a. Determine the value of the elastic modulus for Ti-6Al-4V
at 427° C.
b.Determine the change in length of a for Ti-6Al-4V test
specimen (originally 5 inch long) that is subjected to a tensile
stress of 40,000 lb/in2 at 427° C.
c. Determine the 0.2% YS for TMC at 25° C and 427° C....
Tensile strain is: A) the stress per unit area B) the same as force C) the ratio of stress to elastic modulus D) the applied force per cross-sectional area E) the ratio of the change in length to the original length
Refer to the following figure, stress-strain diagram,
for samples of three different materials: A, B, and C. The end of
each curve indicates the fracture point.
e) After the conclusion of the tests, if the broken halves of each
sample were fitted back together, which sample would be the
shortest? Assume that all three samples had the same initial
length. f) A circular rod is to be produced, 15 cm long with a
diameter of 5.0 mm. This rod must...
A tensile test was conducted on a specimen that had an original diameter of 0.5 in. It fractured with an applied load of 71100lb. Determine the true stress and true strain at fracture if measured diameter of the fracture part was 0.3in. I believe for fracture, true stress and strain are: True strain = ln(original area/final area) True stress = applied load/final area However, Im not quite sure
Problem 6-9
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6. What four factors govern a rock's response to applied stress? a Rate of strain, Temperature, Azimuth, Gradation b. Confinement, Rate of strain, Rock strength, Temperature C. Confinement, Rock strength, Gradation, Weathering d. Temperature, Rate of strain, Dimensions, Faulting 7. The drawing below is a strike-slip fault with offset segments. Identify (1), the lateral motion (right or left lateral), and (2), the step-over direction. Would you expect to see a small normal or reverse fault in...
(30 points) From the stress-strain chart for a unknown material determine thoe following 400 a) The modulus of elasticity b) The yield strength at a strain offset of 0.002 c) Tensile strength d) The Ductility (percentage of 300 200 elongation, %EL) e) The Modulus of resilience f) Strain at 350 Mpa stress g) Strain at 150 Mpa stress 200 100 100 0.005 0.30 0.40 0.10 trein 0.20