AIRCRAFT STRUCTURE I M1 Flashcards

1
Q

The key discovery that “_____” could be created by passing air over
the top of a curved surface set the development of fixed and rotary-wing aircraft in
motion.

A

LIFT

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2
Q

_______ developed an efficient cambered airfoil in the early 1800s, as
well as successful manned gliders later in that century.

A

George Cayley

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3
Q

He established the principles of flight, including the existence of lift, weight, thrust, and drag.

A

George Cayley

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4
Q

It was _____ who first stacked wings and created a tri-wing glider that flew a man in 1853.

A

George Cayley

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5
Q

The term “_____” is often used interchangeably with the word “strain.”

A

STRESS

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6
Q

External loads or forces cause _____.

A

STRESS

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7
Q

____ is a material’s
internal resistance, or counterforce, that opposes deformation.

A

STRESS

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8
Q

The degree of deformation of a
material is ______.

A

STRAIN

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9
Q

When a material is subjected to a ________, that material is deformed,
regardless of how strong the material is or how light the load is.

A

load or force

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10
Q

FIVE MAJOR STRESSES

A
  1. Tension
  2. Compression
  3. Torsion
  4. Shear
  5. Bending
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11
Q

is the stress that resists a force that tends to pull something apart.

A

TENSION

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12
Q

pulling force transmitted axially by the means
of a string, a cable, chain, or similar one dimensional continuous object, or by each end of a rod, truss member, or similar three-dimensional object; tension might also be described as the
action-reaction pair of forces acting at each end of said elements.

A

TENSION

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13
Q

could be the
opposite of compression.

A

TENSION

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14
Q

is the stress that resists a crushing force.

A

COMPRESSION

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15
Q

The compressive strength of a material is also measured in ____.

A

PSI

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16
Q

is the stress that tends to shorten or squeeze
aircraft parts.

A

COMPRESSION

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17
Q

_________ stress is a force that causes a material to deform to occupy a smaller volume.

A

Compressive

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18
Q

stress that produces twisting. While moving the aircraft forward, the
engine also tends to twist it to one side, but other aircraft components hold it on course.

A

TORSION

19
Q

The ______ strength of a material is its resistance to twisting or torque.

A

TORSION

20
Q

is the stress that resists the force tending to cause one layer of a material to slide over an adjacent layer.

A

SHEAR

21
Q

Two riveted plates in tension subject the rivets to a ________ force.

A

SHEARING

22
Q

the ________ strength of a material is either equal to or less than its tensile or
compressive strength.

A

SHEARING

23
Q

Aircraft parts, especially screws, bolts, and rivets, are often subject to a
_____ force.

A

SHEARING

24
Q

______ stress may occur in solids or liquids; in the latter it is related to fluid
viscosity.

A

SHEAR

25
Q

_____ stress is a combination of compression and tension.

A

BENDING

26
Q

In applied mechanics, ________ (also known as flexure) characterizes the behavior of a
slender structural element subjected to an external load applied perpendicularly to a
longitudinal axis of the element.

A

BENDING

27
Q

The airframe of a fixed-wing aircraft consists of the following five major
units:

A

 Wings
 Fuselage
 Stabilizers
 Flight control surfaces
 Landing gear

28
Q

A rotary-wing aircraft consists of the following four major units:

A

 Fuselage
 Landing gear
 Main rotor assembly
 Tail rotor assembly

29
Q

The primary factors to consider in
aircraft structures are ______, _____, and ______.

A

strength, weight, and reliability

30
Q

An aircraft ________ must be strong and light in weight.

A

AIRFRAME

31
Q

All materials used to construct an aircraft must be ______.

A

RELIABLE

32
Q

_________ minimizes the
possibility of dangerous and unexpected failures.

A

RELIABILITY

33
Q

The _______ absorbs the forces imposed on the aircraft by takeoffs and
landings.

A

LANDING GEAR

34
Q

During flight, any maneuver that causes acceleration or deceleration increases the
forces and stresses on the _____ and ______.

A

wings and fuselage

35
Q

The _______ absorbs the same stresses and transmits them to the
fuselage.

A

empennage (tail section)

36
Q

the study of loads is called a ____________

A

stress analysis

37
Q

_____ are analyzed and considered when an aircraft is designed.

A

STRESSES

38
Q

_____ is defined as
pull.

A

TENSION

39
Q

It is the stress of stretching an object or pulling at its ends.

A

TENSION

40
Q

forces acting on an aircraft move toward
each other to squeeze the material,

A

COMPRESSION

41
Q

__________ is the resistance to crushing produced by two forces pushing toward each other
in the same straight line.

A

COMPRESSION

42
Q

cutting a piece of paper with scissors
is an example of a ______ action

A

SHEARING

43
Q

stress exerted when two
pieces of fastened material tend to separate.

A

SHEAR