8.2 Airflow Around A Body Flashcards

1
Q

What is static pressure

A

Stationary

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2
Q

What is dynamic pressure

A

1/2 p x v2

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3
Q

What is Bernoulli’s theorem

A

Total pressure = Static + dynamic

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4
Q

What is a jet outlet

A

When diameter decreases and speed increases

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5
Q

What is a diffuser outlet

A

When diameter increases and speed decreases

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6
Q

What is a Venturi tube

A

Airflow increases when it narrows

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7
Q

What is the boundary layer

A

Is the layer of fluid density above the surface of the skin
It is retarded air

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8
Q

What is laminar flow

A

When particles in fluid all flow parallel to one another
This is desirable as less drag so more fuel efficient and high lift
Flow over the leading edge

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9
Q

What is turbulent flow

A

High pressure in turbulent air
There is more friction drag
High aot cause greater amounts of turbulent flow

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10
Q

What is free stream airflow

A

Air above boundary layer that is unaffected by friction

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11
Q

What is relative airflow

A

Direction of airflow with respect to moving body

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12
Q

Where is transition point of laminar flow

A

Max thickness and lowest pressure where flow separates

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13
Q

What is upwash

A

Air flowing towards the wing will flow upwards to the low pressure upper surface of the wing

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14
Q

What is downwash

A

The fluid flow returns to its original state

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15
Q

What do door gutters help with

A

Reflect upwash and downwash

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16
Q

What are vortices

A

Are circular patterns of rotating air behind a wing
Goes clockwise at left wing tip
Anti-clockwise at right

17
Q

What is the camber line

A

Line that is equidistant from the upper and lower surface
Mid line between top and bottom surface

18
Q

What is chord line

A

Line between the leading and trailing edge
Low speed profile has max camber 5% 45% aft leading egdge

19
Q

What is finess ratio

A

Max thickness of a section expressed as a percentage

20
Q

What is aspect ratio

A

Ratio of wing length to width
High ar = low drag
Low ar = high drag

21
Q

What is washin wings

A

Angle of incedence is greater at wing tip than wing root
Aerodynamically twisted wings are washin

22
Q

What is wash out wings

A

Angle of incedence is greater at the root than the wing tip
These are geometrically twisted

23
Q

What is the mean aerodynamic chord

A

Average chord length of a tapered or swept wing
Centre or lift and centre of pressure act here

24
Q

What is the angle of attack

A

Angle between relative wind and relative chord line

25
Q

What is angle of incedence

A

Angle between the chord line and aircraft centre line

26
Q

What are the wing shapes

A

Elliptical entire wing stalls
Rectangular root stall first nose down
Swept back tip stall first nose up

27
Q

Why are wings swept back

A

To reduce critical Mach number

28
Q

What is induced drag

A

Downwards flow of the wing tip vortice inside the span

29
Q

What is form drag

A

Caused by differences in pressure between leading and trailing edge

30
Q

What is friction drag

A

Inversely proportional to form drag

31
Q

What is interference drag

A

Turbulence in airflow caused by sharp corners
Fairings used to counteract

32
Q

How is lift generated

A

Air circulating around the aerofoil by the Magnus effect

33
Q

What is glide ratio

A

Highest lift to lowest drag at a certain aoa 4 degreees