Exam 1 Flashcards

(55 cards)

1
Q

Engineering Materials

A

Polymers, Ceramics, Metals, Composites

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2
Q

Proton

A

Subatomic particle. Have mass and positive charge

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3
Q

Neutron

A

Subatomic particle. Have mass and neutral charge

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4
Q

Electron

A

Subatomic particle. Have a negative charge.

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5
Q

Valence Electrons

A

Electrons in the outer orbit (shell) of an atom. These electrons largely determine the chemical properties of an element.

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6
Q

Ionic Bonding

A

Chemical bond between atoms in which one atom gives up valence electrons to become a positive ion and another atom gains valence electrons to become a negative ion. Bonded electrostatically.

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7
Q

Covalent Bonding

A

Chemical bond between atoms in which atoms share valence electrons in order to fill the outer electron orbit (shell) of both atoms. This sharing of electrons then bonds the atoms together.

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8
Q

Metallic Bonding

A

Chemical bond between atoms in which atoms give up valence electrons to form an electron matrix (electron cloud) and positive ions. The atoms are bonded together by the electrostatic attraction between the positive ions and the negative electrons on the matrix. “Blank” bonding gives metals their unique characteristics.

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9
Q

Van Der Wall Forces

A

Weak secondary inter-atomic attractions arising from internal dipole effects (electrostatic).

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10
Q

Element

A

A pure substance that cannon be broken down into other substances by chemical means.

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11
Q

Alloy

A

A material that has metallic characteristics and is composed of two or more elements, of which at least one is a metal.

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12
Q

Structure

A

The manner in which atoms are arranged in a metal or alloy.

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13
Q

Chemical Properties

A

Material characteristics related to the structure of a material with each other and with various forms of energy.

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14
Q

Physical Properties

A

Material characteristics pertaining to the interaction of materials with each other and with various forms of energy.

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15
Q

Mechanical Properties

A

Material characteristics that are seen when a mechanical force is applied to the materials.

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16
Q

Service Failures

A

Engineering materials fail in service by one of the following three methods: Corrosion, Wear, or Mechanical Overload

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17
Q

Crystal Lattice Structures

A

Orderly and specific arrangement of atoms in a series of unit cells. Three common metal types are BODY CENTERED CUBIC, FACE CENTERED CUBIC, HEXAGONAL CLOSE PACKED

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18
Q

Amorphous Structures

A

Solid materials that do not have a repeating orderly arrangement of their atoms.

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19
Q

Nucleus

A

The starting point of a crystal grain growth as the metal solidifies.

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20
Q

Dendric

A

The tree-like manner in which a metal crystal grows from he nucleus into the grain during solidification.

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21
Q

Grain

A

Metal crystals with an irregular three dimensional, external shape and an orderly, specific internal atomic arrangement (crystal lattice structure).

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22
Q

Phase

A

A physically homogeneous portion of a material. Has the same structure throughout it, roughly the same composition and properties throughout it, and an interface between it and other phases.

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23
Q

Allotropic Change

A

The change of a metal from one crystal lattice structure to another in the solid state.

24
Q

Dislocations

A

Imperfections on an atomic scale within the crystal lattice structure that allows plastic deformation to occur.

25
Slip Planes
The closest packed atomic planes in the crystal lattice. These are the planes that dislocations move along.
26
Cold Working, Work Hardening, Strain Hardening
Plastic deformation of a metal below the recrystallization temperature. The changes produced by the work on the crystal lattice structure remain as distorted atoms. 1 f the 4 major methods of increasing strength in materials.
27
Hot Working
Plastic deformation of a metal above the recrystallization temperature. The metal is constantly being annealed.
28
Annealing
Three stage process of restoring cold worked metal to its original soft, unstained conduction. The three stages are recovery, recrystallization, and grain growth. This is a softening process.
29
Recrystallization
The lowest temperature at which the distorted grain structure of a cold worked metal changes to a new, strain free non-distorted structure.
30
Stress
Load on a body distributed over the body's cross-sectional area, or force per unit area. (Units of Pascals or psi)
31
Strain
Deformation of a body under stress, measured in units of change in length per unit length. (in/in)
32
Elastic Strain
Strain that disappears on removal of the stress that caused it.
33
Plastic Strain
Strain that remains on removal of the stress that caused it.
34
Elongation
Deformation of a body under stress, measured in terms of total change in length.
35
Static Load
Load imposed without motion, acting by weight alone.
36
Dynamic Load
Load imposed with both weight and motion (impact).
37
Hardness
The ability of a material to resist penetration or indentation. Rockwell and Brinell are common hardness testing methods.
38
Strength
The material's ability to resist deformation (or fracture) from applied stress.
39
Plasticity
The ability of a material to deform without fracture. Two types of plasticity are Ductility and Malleability.
40
Brittleness
The tendency of a material to fracture suddenly without plastic deformation. The opposite of plasticity.
41
Yield Strength
The stress that will produce a specified amount of plastic strain in a material.
42
Modulus of Elasticity
Measure of resistance to elastic deformation. The higher the modulus of elasticity, the lower the amount of strain for a given amount of stress, and the more "elastically stiff" the material.
43
Elastic Limit
The point in tensile loading where strain is no longer proportional to the applied stress. (end of elastic region)
44
Ductility
Plasticity of a metal under tensile stress.
45
Malleability
Plasticity of a metal under compressive stress.
46
Toughness, Impact Strength
The ability of a metal to absorb energy without fracture. Toughness is a combination of strength and ductility. Izod and Charpy...
47
Resilience
The ability of a metal to absorb energy without plastic deformation. Combination of strength and elasticity.
48
Shear Strength
The stress required to produce fracture in a plane of the cross section of the material.
49
Creep Strength
The constant nominal stress that will cause a specified quantity of creep in a given time at a specified temperature.
50
Fractures or Failures
4 common mechanical types of overload fractures are brittle, ductile, fatigue and creep.
51
Endurance Limit
The maximum stress below which a material can withstand an infinite number of stress cycles. Steels and Titanium alloys have endurance limits.
52
Fatigue Strength
The stress that will cause fatigue fracture after a set number of stress cycles. Used for Aluminum alloys and other non-ferrous metals.
53
Why do atoms bond?
To reach their lowest energy state
54
Common Crystal Defects
Vacancy and Dislocation
55
D.B.T.T.
Ductile to Brittle Transition Temperature