Air Flow Flashcards

1
Q

What is the COANDA effect

A

When the flow of air encounters an object in its path it attaches itself to the objects surface and flows smoothly around it.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

2 conditions for the COANDA effect

A

The object is presented to at the airflow at aa slight angle.

The objects shape is relatively thin and smooth.(streamlined).

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

Why does high pressure attract to low pressure

A

Air naturally goes from areas of high pressure to low pressure.Areas of depleted molecules need filling.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

What is a pressure gradient

A

Differences in pressure over a distance.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

What are streamlines/streamtube.

A

Streamlines are directions of flowing air .

A volume of air bounded by streamlines.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

What are the three types of flow

A

Laminar flow,
Turbulent flow,
Vortex flow

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

What is laminar flow/streamlined flow

A

Laminar flow is when airflow moves from one direction to another in layered predicable flows. Smooth and predictable.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

Turbulent Flow

A

Air flowing past unstreamlined object breaks the streamlined flow resulting in an unsteady or turbulent flow. Forms a resistant to the streamlined flow that becomes drag.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

Vortex flow

A

Loses energy as it moves away from aircraft. Caused by aircraft itself from drag.

All 3 types of flow moving around aircraft at same time

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

What is an ideal fluid

A

Has 2 key properties.
It is incompressible (density does not change))
Has no Viscosity.
Air is known as an ideal fluid.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

Equation of continuity in relation to mass flow

A

Mass can neither be destroyed nor created. Mass flow must remain the same (E.g when entering a streamtube)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

Relationship of area and Volume in a Venturi

A

A1XV1=A2XV2=A3XV3

When A2 decreases V2 increases
When A3 increases V3 decreases.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

Speed at which air density does not change

A

Upto 300knots

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

Venturi Tube

A

Mass Flow entering must remain same exiting. At the throat of a Venturi flow rate increases as cross section area decreases.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

Relationship between airflow velocity and distance between streamlines

A

Spacing between stream lines reduces as flow velocity increases and increases when flow velocity decreases.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

Law of conservation of energy

A

Energy can neither be destroyed nor created only change from one form to another. Bernoulli’s theorem energy in a flow must remain constant.

17
Q

Bernoulli Principle

A

In the flow of an ideal fluid, the sum of pressure (static)and kinetic energy(dynamic pressure) must remain constant. Energy in a flow must remain constant.

18
Q

Converging Airflow (Venturi)

A

As tube converges flows speed increases. Dynamic pressure increases and static pressure decreases by
the same proportions.

In a diverging flow the opposite occurs.

SAME TOTAL PRESSURE MIST ME MAINTAINED.