8.2 Flashcards

1
Q

Unit for KInetic energy

A

KE = 0.5 *p * V^2
Unit is joules

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2
Q

What is the principle of continuity

A

Energy or mass can’t be created or destroyed it can only be changed from 1 form to anoth3r

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3
Q

What is laminar flow

A

When there is a smooth regular airflow pattern around an object

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4
Q

What is turbulent flow

A

This happens when air is disturbed and separates from the surface of a moving body

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5
Q

State the continuity equation what is the mathematical expression

A

States that the speed of the airflow is inversely proportional to the area of the cross section of the tube if the density remains constant

p1=p2 (density)
Therefore
V1 * A1 = V2 * A2

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6
Q

What is boundary layer

A

Is the layer of fluids in the immediate area of a surface

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7
Q

What is known as the no slip conditions

A

This is when the surface brought to rest by friction

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8
Q

As an aircraft moves through the air it affects the air around it. What are the causes for this

A

Change in direction, Heat up, changing velocity and pressure

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9
Q

As an aircraft moves through the air it affects the air around it. What are the causes for this

A

Change in direction, Heat up, changing velocity and pressure

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10
Q

Advantages of laminar flow

A

Laminar flow has less surface friction giving rise to low fuel usage, giving greater range.

Ability to glide further in the event of engine failure.

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11
Q

Disadvantages of laminar flow

A

Low kinetic energy this means easier for flow separation to occur. Easier to stall at lower angles of attack.

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12
Q

What is a vortices

A

Circular pattern of rotating air is formed behind a wing or control surface as it generates life or force from the pressure differential

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13
Q

What is stall

A

Reduction in lift when AOA is reached

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14
Q

What are the 2 type of stall

A

Wing root stall
Wing tip stall

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15
Q

What is a stall strip

A

It’s used on smaller aircraft to prevent wings tip from stalling first

It’s mounted at the leading edge of the wing root and the disadvantage is it disturbs the lift

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16
Q

What is a slat

A

It’s to prevent wing tip stall on some larger aircraft. Slats extends automatically if THE AOA is goo high

Located at the leading edge of the wing tip

17
Q

What are slots

A

It opens up and the boundary layer is energised which prevents flow separation

18
Q

What are 3 types of ice

A

Frost
Rime ice
Clear ice

19
Q

What happens when there is a build up of ice

A

Affects the aircrafts performance such as extra weight, more drag, loss of lift

20
Q

Whats determined when your in a forward motion

A

Thrust and drag