Sample Midterm/Final Questions Flashcards
At 548 degrees celsius, aluminum can dissolve up to 6% copper as a substitutional solid solution. If this alloy is quenched in water to room temperature:
a) It becomes a super-saturated solid solution of aluminum of aluminum which can be further heat treated by aging to optimize the alloy’s mechanical properties.
b) The copper atoms squeeze into the spaces between the aluminum atoms but precipitate out of solution upon quenching.
c) The crystal structure is basically that of FCC aluminum with some of the aluminum atoms replaced by CuAl2.
d) The structure consists of grains of pure aluminum which makeup 94% of the weight of the material. The remaining 6% of the weight occurs as grains of pure copper.
e) The crystal structure of the solid so
a) It becomes a super-saturated solid solution of aluminum of aluminum which can be further heat treated by aging to optimize the alloy’s mechanical properties.
from Parv pack, p.1
Which of the following may occur during an annealing heat treatment of a previously cold-worked alloy?
a) Internal stresses may be relieved.
b) Ductility will increase.
c) Toughness may increase.
d) A new microstructure may be produced.
e) All of the above.
e) All of the above.
from Parv pack, p.1
Your company tells you to increase the factor of safety (N) for a component that has a working load of 20 kN. The component must not deform permanently under load. Which of the following changes would increase the factor of safety?
a) increasing the tensile load on the component
b) selecting a material with smaller work hardening coefficient (n)
c) decreasing the cross sectional area of the component
d) changing to a material with a higher yield strength
e) the safety factor is a constant that cannot be changed
a) or d)
from Parv pack p.2 & 22
A cylindrical specimen of a metal alloy of 48.5 mm long and 9.72 mm in diameter is stressed in tension. A true stress of 393 MPa causes the speciment to uniformly plastically elongate to a length of 57.2 mm. If it is known that the strain-hardening exponent for this alloy is 0.20, calculate the true stress (in MPa0 necessary to plastically elongate a specimen of this same material from a length of 48.5 mm to a length of 54.7 mm.
a) 253
b) 368
c) 433
d) 529
e) 563
using true stress equation
b) 368
from Parv pack p.2 & 22
A copper matrix is reinforced with 20% tungsten particles. The modulus of elasticity for copper is 110 GPa and that for tungsten is 407 GPa. Estimate the minimum modulus of elasticity for the composite material.
a) 348 GPa
b) 264 GPa
c) 169 GPa
d) 129 GPa
e) 52 GPa
using composite material formula for E
d) 129 GPa
from Parv pack p.3
For a particular metal of σo=0, the grain size increases from 35 X 10-6 m to 70 X 10-6 m, the yield strength changes in the following way:
a) it decreases by a factor of 1.41
b) it increases by a factor of 1.41
c) it does not change
d) it decreases by a factor of 4
e) it increases by a factor of 4
a)
from Parv pack p.3 & 17 and another page too
Which of the following statements is correct? For a cold worked material:
a) The higher the amount of prior cold work, the lower the recrystallization temperature.
b) The higher the melting temperature of the material, the lower the recrystallization temperature.
c) The density of dislocations increases with increasing temperature.
d) The longer the time of heating, the higher the recrystallization temperature.
e) Pure materials recrystallize at higher temperatures than solid solutions.
a)
from Parv pack p.3&17&another
The elastic moduli in the 0 degree and the 90 degree directions of a unidirectionally reinforced composite (e.g. unidirectional carbon fibres in an epoxy matrix) can be calculated using the iso stress and iso-strain models. These models assume that:
a) The fibres are free to slide in the matrix
b) When the fibres are loaded in the iso-train case, the fibres and matrix both elongate by the same amount
c) When the fibres are loaded in the iso-stress case, the fibres and matrix both carry the same load
d) Answers (b) and (c) are correct
e) Answers (a), (b), and (c) are correct
d) or e) or B)?
from Parv pack p.4 & 18 and another
In order to form tempered martensite in medium and high carbon steels, the correct heat treatment involves:
a) heat into the martensitic region and slowly cool to room temperature
b) heat into the austensitic region, quench and temper at 200 degrees - 600 degrees
c) heat into the austensitic region, quench and temper at 800 degrees.
d) heat into the ferritic region, quench and temper between 200 degrees - 600 degrees
e) heat into the martensitic region, quench and temper between 200 degrees - 600 degrees
d) heat into the ferritic region, quench and temper between 200 degrees - 600 degrees (but fact check this answer!!!)
from Parv pack p.4 & 18 &other
With reference to the Charpy impact test, which of the following statements is true?
a) FCC metals typically show a strong dependence of impact energy absorbed as a function of test temperature
b) High strength metals always show high toughness and are not affected by test temperature
c) The Ductile-Brittle transition refers to the impact speed when the metal can no longer deform plastically
d) The Ductile-Brittle transition temperature occurs at a fixed temperature for a given metal (like a melting point)
e) For a structural steel, a lower Ductile-Brittle transition temperature is desirable
d) The Ductile-Brittle transition temperature occurs at a fixed temperature for a given metal (like a melting point) (or e), check!)
from Parv pack p.4 & p.19
Which of the following statements concerning dislocations is false?
a) In an edge dislocation, b, the Burger’s vector, is parallel to the slip direction
b) In a screw dislocation, b, the Burger’s vector, is parallel to the slip direction
c) In an edge dislocation, b, the Burger’s vector, is perpendicular to the dislocation line
d) In a screw dislocation, b, the Burger’s vector, is perpendicular to the dislocation line
e) Both edge and screw dislocations can cause slip.
b) or e) or D?
from Parv pack p.5 p. 19
Which of the following strengthening methods for metals and alloys is best suited for high temperature applications?
a) grain size reduction
b) strain hardening
c) dispersion strengthening
d) precipitation hardening
e) None of the above as the metals will recrystallize
c) dispersion strengthening
or maybe d? check in notes
from Parv pack p.5
Which of the following statements is false?
a) The driving force for recrystallization is the difference in internal energy between the strained and unstrained material.
b) Prior cold working is essential for recrystallization.
c) Recrystallization removes dislocations which restores the ductility of the metal, without changing the size of the grains.
d) Recrystallization is a function of temperature and also a function of time at that temperature.
e) Cold working results in a change of grain shape, an increase in hardness and strength and an increase in dislocation density.
c) is false, the grains get finer
from Parv pack p.5, p.20
The heat treating of steels (quenching and tempering) can be used to change some of the mechanical properties of the steel. This process can be described as:
a) a softening of the material during quenching, followed by a hardening treatment during tempering.
b) a “freezing in” of the soft, annealed microstructure, followed by the formation of martensite during tempering.
c) the formation of hard martensite during quenching, followed by a controlled softening during tempering.
d) the formation of a martensitic phase on quenching which gets harder with tempering
e) a recrystallization process that removes all dislocations followed by controlled deformation during tempering to increase the yield strength
c) the formation of hard martensite during quenching, followed by a controlled softening during tempering.
from Parv pack p.6, p.20
A metal obeys the Hollomon relationship and has K = 581 MPa and n = 0.3. Knowing that the true strain at the onset of necking has a value equal to n, what is the true stress for this metal at this point?
a) 405 MPa
b) 175 MPa
c) 300 MPa
d) 581 MPa
e) 1.9 GPa
using the true stress equation
a) 405 MPa
from Parv pack p.6, p.20
True or False:
When subjected to torsion, a brittle specimen breaks along planes perpendicular to the direction in which tension is a maximum, i.e., along surfaces at 45 degrees to the shaft axis whereas a ductile material fails along planes parallel to planes of maximum shear stress.
True
(Brittle materials are weaker in tension than in shear)
from Parv pack p.7