Properties of Metal Flashcards

(33 cards)

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.

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.

24
Q

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

A

heat-treating or work-hardening, annealing

25
describes a material's tendency to break or shatter when exposed to stress, and is the opposite of ductility and malleability
Brittleness
26
A material's ability to be bent, formed, or shaped without cracking or breaking
Malleability
27
The ability of metal to be drawn into wire stock, extrusions, or rods
Ductility
28
a material's ability to resist tearing or breaking, when it is bent or stretched
Toughness
29
describes a metal's tendency to return to its original shape after normal stretching and bending
Elasticity
30
the property which enables a metal to carry heat or electricity
Conductivity
31
The property of a metal to expand when heated and shrink when cooled
Expansion and Contraction
32
The ability of metal to be joined by heating and melting is
Fusibility
33
material's mass per unit volume.
Density