Stress Analysis (Machine Design 1) Flashcards

1
Q

a stress that is mainly due to a force applied to a machine member in which the resisting area is normal or perpendicular to the direction of the force.

A

Normal Stress

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2
Q

a stress caused by a force in which the resisting area is parallel to the direction of the force

A

Shear Stress

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3
Q

a type of compressive stress which involves two members in contact; also referred as contact stress.

A

Bearing Stress

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4
Q

Every direct stress is accompanied by a strain in its own direction which is known as

A

linear strain

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5
Q

an opposite kind of strain in every direction, at right angles to it, is known as

A

lateral strain

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6
Q

It has been found experimentally that when a body is stressed within elastic limit, the lateral strain bears a constant ratio to the linear strain

A

Poisson’s Ratio

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7
Q

When a body is subjected to two equal and opposite forces acting tangentially across the resisting section, as a result of which the body tends to shear off the section, then the stress induced is called

A

shear stress

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8
Q

When a machine member is subjected to the action of two equal and opposite couples acting in parallel planes (or torque or twisting moment), then the machine member is said to be subjected to

A

torsion

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9
Q

The stress set up by torsion is known as

A

torsional shear stress

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10
Q

if the deformation of the body is prevented to occur due to
some restrictions, some stresses are induced in the body. Such stresses are known as ______________.

A

thermal stresses

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11
Q

states that when a material is loaded within elastic limit, the stress is directly proportional to strain

A

Hooke’s Law

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12
Q

It is defined as that stress at which the stress-strain curve
begins to deviate from the straight line.

A

A=proportional limit

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13
Q

It is defined as the stress developed in the material without any permanent set.

A

B=elastic limit

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14
Q

If the material is stressed beyond point B, the plastic stage will reach i.e. on the removal of the load, the material will not be able to recover its original size and shape.

A

C and D=upper and lower yield points

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15
Q

The stress has attained its maximum value known as ultimate stress. It is defined as the largest stress obtained by dividing the largest value of the load reached in a test to the original cross-sectional area of the test piece

A

E= ultimate point

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16
Q

After the specimen has reached the ultimate stress, a neck is formed, which decreases the cross-sectional area of the specimen. A little consideration will show that the stress (or load) necessary to break away the specimen, is less than the maximum stress. The stress is, therefore, reduced until the specimen breaks away at point F. The stress corresponding to point F is known as breaking stress.

A

F=breaking stress

17
Q

It is defined, in general, as the ratio of the maximum stress to the working stress.

A

Factor of Safety or Design Factor