Stress and Sound Flashcards

1
Q

Stress

A

An internal force in an object which resists any attempt by an external force to change the shape of the object

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2
Q

Types of Stress

A

Tension

Compression

Shear

Torsion

Bending

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3
Q

Tension

A

A stress that tries to pull an object apart

Two forces acting in the opposite direction outward, along the same line

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4
Q

Compression

A

A stress that tries to push an object together

Two forces acting in opposite direction inward, along the same line

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5
Q

Shear

A

A stress that tries to slide objects apart

Two forces acting in opposite direction (inward or outward) along different lines

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6
Q

Torsion

A

A twisting force

Two forces applied in opposite direction, along the same axis

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7
Q

Bending

A

A combination of tension, compression, and shear

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8
Q

Strain

A

The deformation of a material caused by stress

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9
Q

Elasticity

A

The property of a material to return to its original shape after being placed under an external stress

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10
Q

Elastic Limit

A

The greatest external stress an elastic solid can sustain without undergoing permanent (plastic) deformation

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11
Q

Yield Point

A

The point where a material will continue to deform without applying additional force other than gravity

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12
Q

Ultimate Strength

A

Point where the part will break

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13
Q

Hook’s Law

A

Stress is equal to strain until the elastic limit is exceeded

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14
Q

Requirements for Sound to Exist

A

Source

Transmission medium

Receptor

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15
Q

Waves

A

Consists of crests and troughs

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16
Q

Wave Length

A

The distance between crests

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17
Q

Cycle

A

One complete crest and trough

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18
Q

Frequency

A

The number of cycles that pass a given point in one second

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19
Q

Frequency Measurement Units

A

Hertz

One Herts is equal to one cycle per second

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20
Q

Speed of Sound

A

Changes as both the density and the temperature of the medium changes

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21
Q

Speed of Sound and Density

A

The speed of sound is directly proportional to the density of the transmission medium

Sound travels 15 times faster through steel as it does through the air

22
Q

Speed of Sound and Temperature

A

The speed of sound is directly proportional to the temperature of the medium

The speed of sound will change by 1.1 fps. For each degree of Farhenheit temperature change

23
Q

Speed of Sound at Sea Level Under Standard Conditions

A

1116 fps = Mach 1
761 mph = Mach 1

24
Q

Subsonic

A

True airspeed less than Mach 1

25
Mach Critical
.72-.85 subsonic airspeed The subsonic airspeed at which a shock wave will start to develop on an aircraft's wing horizontal stabilizer and cockpit
26
Transonic
True airspeed passing through Mach 1
27
Supersonic
True airspeed above Mach 1
28
Doppler Effect
A frequency shift caused by the relative motion between the source and receptor
29
Fuselage
Main body of the aircraft
30
Truss
Pratt truss Warren truss
31
Pratt Truss
Box like frame Not very strong
32
Warren Truss
Triangular frame Strongest truss type frame
33
Monocoque (4)
Old metal and wood covered aircraft Skin is stretched around vertical members called rings and formers Skin gives the structure strength, holds the fuselage rigid and requires a thick skin Dents, cracks cause a rapid failure
34
Semi-Monocoque
Most modern metal covered aircraft are of this type Along with the vertical. This structure also incorporates longitudinal members called longerons - Longerons and stingers - Bending loads are taken up the longitudinal members. Therefore, skin thickness can be reduced
35
Bulkheads
Used attachment points, and pressurization sections
36
Rings and Formers
Hold the fuselage and shape
37
Longerons
Heaviest members extends across several vertical members Takes up primary bending load
38
Stringers
Lightweight, maintain shape of the structure
39
Guessets
Used at the intersection of vertical and horizontal members Add strength and stiffness to the airframe
40
Aircraft Skin
Monocoque and semi-monocoque aircraft have stressed skin Skin is under constant tension, compression, bending and torsion loads NOTE: Even small cracks are critical
41
Pylons
Provide mounting points for engines and external stores
42
Nacelles
Smooth airflow and reduce the drag around engines, fuel tanks, etc...
43
Wings
Main lifting body of the aircraft May be designed to house wheels, supports, contain fuel, mount flight controls, etc...
44
Metal Wings
During flight, wing is subject to bending loads Lower skin more critical to repar than lower wing (look up and confirm in book) Lower skin under a tension load Upper skin under a compression load
45
Semi-Cantilever
Requires extra bracing
46
Landind Struts
On a low wing aircraft
47
Lifting Struts
On a high wing aircraft
48
Cantilever wing
Requires no external bracing and has a heavy constructed center section
49
Spars
Runs the span of the wind from the wing root to the wing tip The principal structural component of the main load bearing member Wings may have a single or multi-spar design
50
Wings contain
Spars, ribs, stringers, and bulkheads
51
Wing Covering Materials
Metal Composite material Doped fabric Plywood