a) PMMA
As we can see from graph PMMA has endurance limit of 10Mpa.
b) True
Sharper cracks are more vulnerable and hence effect KIC.
c) 246mm

4 a) 4 a) continued b) c) Based on the following figures, the material that exhibits...
5 a)
b)
c)
d)
The size of an internal crack that can be tolerated in alloy steel 4340 tempered at 425C for a stress of 100 MPa is (use any needed data from Chapter 8): 487 mm 80.5 mm O 246 mm 40.25 mm 161 mm 287 mm 492 mm 368 mm 122 mm 413 mm The fatigue strength after 100 million cycles in 2014-T6 aluminum alloy is (see the figure shown below): 700 600 Ti-5Al-2.5Sn titanium alloy 4340...
A cylindrical bar of ductile cast iron is subjected to reversed
and rotating-bending tests, test results (i.e., S-N
behavior) are shown in Animated Figure 8.21. If the bar diameter is
8.52 mm, determine the maximum cyclic load that may be applied to
ensure that fatigue failure will not occur. Assume a factor of
safety of 2.21 and that the distance between loadbearing points is
55.3 mm.
answer in N
We were unable to transcribe this imageReferences Cycles to failure 3.2E...
Q-1. You are testing a circular beam of two metals, 1045 steel and 2014-T6 aluminum, in a rotating-cantilever beam fatigue test. If you need to choose one of these metals so that you can essentially design a part made of that metal, and subject the part to a repetitive stress- amplitude without ever failing due to fatigue, which one would you choose. (See the attached figure) 700 600 Ti-5Al-2.5Sn titanium alloy 4340 steel 500 400 Maximum stress, S (MPa) 1045...
1 a)
b)
Which polymers in the following figure does NOT show a clear endurance limit (select the best answer)? 25 PS PET 3 20 15 PMMA 2 Stress amplitude (MPa) Stress amplitude (ksi) 10 PP. Nylon (dry) 1 PE 5 PTFE 103 104 105 106 107 Number of cycles to failure PS PMMA PP PET O PE Which of the following materials is likely to have the highest Kic? inorganic window glass Rubber tyre O Nylon polycarbonate Concrete O...
A 6.4 mm diameter cylindrical rod fabricated from a 2014-T6 aluminium alloy is subjected to reversed tension-compression load cycling along its axis of +7400 N to -2250N. Determine the fatigue life using the data shown below. 500 400 1045 steel 300 2014-T6 aluminum alloy 200 100 Red brass 10 103 104 106 105 108 10° 1010 Cycles to failure, N Stress amplitude, S (MPa)
A 6.4 mm diameter cylindrical rod fabricated from a 2014-T6 aluminium alloy is subjected to reversed...
Qu.2 Chapter 8: Failure (2096) crack of length of 1.0 mm was detocted on the surface of the shaft of wind turbine (see Figure 3), made from 4340 steel. The diameter of the shaft of wind turbinc is cqual to 30 mm. Assuming subjected to a maximum load of 20,000 N during operation. 10.2 mm and Y ?! the radius of the curvature of the crack is 1x What is the maximum stress(o.) experienced by the shaft during operations? (a)...
Q6. (a) Three identical fatigue specimens (denoted A, B and C) are fabricated from a non-ferrous alloy. Each is subjected to one of the maximum- minimum stress cycles listed in Table 26 (the frequency is the same for all tests) Table 26 Specimen Omax (MPa) Omin (MPa) A +450 -150 +300 -300 +500 -200 Rank the three specimens in terms of their fatigue lifetimes (highest to lowest). Justify this ranking [5 marks] (b) A cylindrical tie rod of diameter 20...