11.3 Wings Wing Construction Flashcards

1
Q

What does the design of a wing depend on ?

A

-size
-weight
-use of aircraft
-speed in flight
- desired rate of climb
-landings

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2
Q

What design are the majority of aircraft wings?

A

Full cantilever design

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3
Q

What is a full cantilever design

A

They do not need external members as all structural members are supported by the skin

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4
Q

What wing design do most small aircraft use ?

A

Semi cantilever design

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5
Q

What is a semi cantilever design ?

A

When external struts or wires are used to support the wing and carry aerodynamic loads and landing loads

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6
Q

What are wing support cables and struts usually manufactured from ?

A

Aluminium

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7
Q

What structural components are a wing constructed of?

A

-spars
-stringers
-ribs
-formers

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8
Q

What is the primary structural element of the wings ?

A

-spars

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9
Q

What carries loads during flight?

A

Skin transfers stresses to the ribs then to the spars which bear all the loads during flight

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10
Q

What are three wing construction designs ?

A

-mono spar
-multi spar
-box beam

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11
Q

What is a mono spar construction ?

A

-one main spar ribs or stringers supply shape to the aerofoil

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12
Q

What is a multi spar construction ?

A

Multiple spars are used, ribs and stringers are used for shape.

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13
Q

What is box beam construction?

A

Two main spars with connecting stringers to provide extra strength and shape to the wing

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14
Q

What is a spar?

A

Main structural member of the wings, they are placed parallel to the lateral axis

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15
Q

how are the wing usually attached ?

A

Either a series of
-Wing fittings,
-plain beams,
-truss

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16
Q

What is the most common spar shape ?

A

The I beam

17
Q

What is the top and bottom of an I beam called?

A

The caps

18
Q

What is the vertical member of the I beam called ?

A

The web

19
Q

What are the ribs ?

A

Ribs are the structural piece that runs parallel to the spars. They extend from trailing to leading edge they provide shape to the aerofoil

20
Q

What are false ribs ?

A

Ribs that do no span the entire length of the wing chord

21
Q

Where can wing butt ribs be found ?

A

At the inboard edge of the wing (the root)

22
Q

Where the wing attaches to the centre wing box, what is it usually covered with ?

A

Fairings do achieve smooth airflow over the area

23
Q

Why might wing tips be removable ?

A

They are prone to damage especially on the ground, so they need to be able to be easily replaced

24
Q

What is it called when the skin as well as the spars and ribs are designed to take loads?

A

Stressed skin design

25
Q

In stressed skin design, what might be done to the skin?

A

The skin is stiffened

26
Q

How can a single sheet of aluminium have varying thicknesses ?

A

By chemically milling

27
Q

In an aircraft with stressed skin design, what material may be used ?

A

Honeycomb composites as they are strong and lightweight