Properties of Metal Flashcards

1
Q

It is determined by the percentage of parent metal and other elements used to make an alloy.

A

metal’s strength

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2
Q

Stress Strain Curve
U -
R -
Y -
E -
P -

A

Ultimate Strength
Rupture Strength
Yield point
Elastic limit
Proportial limit

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3
Q

It is the maximum tensile load per unit area which a material can withstand

A

Tensile Strength

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4
Q

It is the ability of metal to resist deformation.

A

Yield Strength

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5
Q

It is the maximum stress a material can
sustain without rupture.

A

Ultimate Strength

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6
Q

It is the maximum stress expected in any
structural member.

A

Limit Strength

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7
Q

describes a metal’s ability to
resist opposing forces.

A

Shear Strength

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8
Q

the ability of a joint to withstand any
form of crushing or excessive compressive distortion.

A

Bearing Strength

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9
Q

It is defined as a material’s ability to resist
deformation under load.

A

Flexural Strength

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10
Q

is the greatest stress a material can withstand without a permanent deformation remaining
upon complete release of the load.

A

Elastic Limit

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11
Q

is the load per unit are acting on a materials

A

Stress

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12
Q

is the deformation of a material caused by an applied load

A

Strain

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13
Q

is the greatest stress at which strain (deformation) is directly proportional to
stress.

A

Proportional Limit

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14
Q

is a stress a material can withstand without resulting in permanent elongation of more than 0.0001 inch per inch of gage length after complete release of stress.

A

Proof Stress

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15
Q

– is the difference in gage length before being subjected to any strength and after rupture.

A

Elongation

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16
Q

– is the difference between the original cross-sectional area and the least cross-sectional area after rupture.

A

Reduction of Area

17
Q

This is any strain remaining after removing the stress.

A

Permanent Set

18
Q

– is the ratio of ultimate stress to limit stress. For nearly all aircraft design, the ultimate factor is 1.5

A

Ultimate Factor (Factor of Safety)

19
Q

– ultimate factor minus 1

A

Margin of Safety

20
Q

– the ratio of maximum to minimum stress applied in one cycle of loading in fatigue test.

A

Stress Ratio

21
Q

– is the ratio of applied load per deformation

A

Stiffness Ratio

22
Q

– is the ratio of lateral strain to axial strain

A

Poisson’s Ratio

23
Q

refers to its ability to resist cutting,
penetration, or abrasion.

A

Hardness

24
Q

Some metals are hardened through ________ ,
while others are softened by a process called
__________.

A

heat-treating or work-hardening, annealing

25
Q

describes a material’s tendency to break or shatter when exposed to stress, and is the opposite of ductility and malleability

A

Brittleness

26
Q

A material’s ability to be bent, formed, or shaped
without cracking or breaking

A

Malleability

27
Q

The ability of metal to be drawn into wire stock,
extrusions, or rods

A

Ductility

28
Q

a material’s ability to resist tearing or breaking,
when it is bent or stretched

A

Toughness

29
Q

describes a metal’s tendency to return to its
original shape after normal stretching and bending

A

Elasticity

30
Q

the property which enables a metal to carry
heat or electricity

A

Conductivity

31
Q

The property of a metal to expand when heated and shrink when cooled

A

Expansion and
Contraction

32
Q

The ability of metal to be joined
by heating and melting is

A

Fusibility

33
Q

material’s mass per unit volume.

A

Density