M8 Revistion Flashcards

(62 cards)

1
Q

Equation for Acceleration

A

Velocity change / time taken

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2
Q

Gravitational acceleration speed

A

9.8 meters per square second

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3
Q

Equation for force

A

Mass * Acceleration

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4
Q

Equation for weight

A

Mass * gravity

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5
Q

Equation for work done

A

Force * Distance

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6
Q

Equation for power

A

Force * Distance
/time

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7
Q

What is Pressure

A

The force acting on a unit of area.

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8
Q

Equation for static pressure

A

Height * Density * Gravity

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9
Q

Equation for Dynamic Pressure

A

Density * 0.5 * Speed^2

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10
Q

Equation for Pressure

A

Force / Area

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11
Q

How does speed of sound relate to temperature

A

The speed of sound is lower at lower temps and higher at higher temps.

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12
Q

Equation for Mach Number

A

Speed of Aircraft / Speed of Sound

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13
Q

What is Subsonic

A

Aircraft speed is below the speed of sound

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14
Q

What is Transonic

A

The aircraft speed is at the speed of sound

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15
Q

What is supersonic

A

Aircraft speed above the speed of sound

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16
Q

What is troposphere

A

The lowest layer where weather forms

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17
Q

What is staposhere

A

The heights level where there no weather and the temp stays the same

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18
Q

Tropopause

A

The boundary between the staposhere and the troposphere

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19
Q

What does I.S.A. stand for

A

International Standard Atmosphere

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20
Q

What are the ISA’s

A

288K
1.225 ks/m^2
-6.5K/1000m
1013.25Hpa

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21
Q

When is air Incompressible

A

When flight is in the subsonic region

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22
Q

Continuity equation states

A

The speed of the airflow is inversely proportional to the area of the cross section

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23
Q

What is a diffuser outlet

A

When the diameter increases and the speed decreases

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24
Q

What is a jet outlet

A

When the diameter decreases and the speed increases

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25
Equation for Totle Pressure
Static pressure + dynamic pressure
26
When is Bernoullis principle used
To measure airspeed
27
What is Magnus effect
When the pressure on the top of the wing is equal to the bottom of the wing.
28
What is profile
The cross section of the wing
29
What is the chord line
A straight line connecting the leading edge to the trailing edge
30
What is the mean camber line
A line drawn between the upper and lower surfaces of the profile
31
What is camber
The displacement of the mean camber line from the chord line
32
What i# fineness ratio
The fraction which determines the thickness of the wing profile
33
What is flight path velocity
The speed of the aircraft in a curtain direction through the air
34
What is relative wind
The speed and direction of the air acting on the aircraft
35
What is Angle of attake
The angle between the chord line and the relative wind
36
What is positive sweep
Wings pointing backwards
37
What is negative sweep
Wings pointing forwards
38
What is dihedral angle
Wings pointing up (Positive dihedral)
39
What is Anhedral Angle
Wing pointing down (Negative Dihedral)
40
What are the 2 components of aerodynamic forces
Lift and Drag
41
Equation for theoretical lift
1/2 * p * v^2 * a
42
Equation for coefficient of lift
Measured lift / theoretical lift
43
Benefit of a thick profile wing
It can fly at slower speeds as it has a lower stall speed
44
Disadvantage of a thick profile wing
Produces more drag and has a lower Mach Number
45
What is centre of pressure
The point where all forces and pressures act
46
Lift and drag depend on:
Surface area of profile Dynamic pressure Shape of profile Edge of attack
47
What are the effects of ice on the wing
Reduces the maximum coefficient and maximum angle of attack
48
What is a polar diagram
Shows how lift and drag coefficients can be combined
49
What is induced drag
Drag on the wing caused by lift
50
What is parasite drag
Drag caused by aerodynamic interference
51
What is compressible drag
Drag caused by a shockwave of an aircraft approaching the speed of sound
52
What is the purpose of wingtips
To reduce induced drag
53
What is form drag
When the pressure in front is different to the pressure behind.
54
How to reduce form drag
By streamlining the aircraft E.g. retracting the landing gear
55
What is interference drag
The turbulence In the airflow caused by the sharp corners of components joined together
56
How can interference drag be reduced
Use of fairings
57
What are the 4 types of wing
Elliptical wing Rectangular wing Tapered wing Swept wing
58
What is aerodynamic centre
A point on the chord line where the magnitude of the pitching moment doesn’t change
59
What is centre of lift
When the CL is in font of the C.G. the nose is pitched up and when the CL is behind the C.G. nose is pitched down
60
What is the mean aerodynamic chord
The average chord length of a wing
61
What is stall
When the angle of attack increases beyond a curtain point that lift begins to decrease.
62
What are the 3 types of stall
Deep stall Wing root stall Wing tip stall