The Basics Flashcards

1
Q

What’s the unit for mass?

A

Kg

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2
Q

What’s the unit for Force?

A

Newton (N) force that accelerates 1Kg at 1m/sec^2

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3
Q

What’s the unit for Time?

A

Seconds

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4
Q

What’s the unit for Distance?

A

Metres

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5
Q

What’s the unit for Area?

A

Metre squared m^2

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6
Q

What’s the unit for Velocity?

A

m/sec

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7
Q

What’s the unit for acceleration?

A

m/sec^2

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8
Q

What’s the unit for Temperature?

A

Kelvin (K)

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9
Q

What’s the unit for pressure?

A

Pascal (Pa): a pressure of 1 N/m^2

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10
Q

What’s the unit for density?

A

Kilograms per cubic metre Kg/m^3

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11
Q

What’s the unit for Energy?

A

Joule = 1 N moving 1 metre

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12
Q

What’s the unit for power?

A

Watt (w): a rate of energy use of 1J/sec

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13
Q

How much is an hectopascal?

A

100 pascals = 1mb

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14
Q

How much is 1 Kg weight into N?

A

9.81 N

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15
Q

What’s Newton’s First Law?

A

A body will continue in a state of rest or uniform motion unless acted on by an external force

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16
Q

What’s Newton’s Second Law?

A

the rate of change of momentum of a body is proportional to the applied force, and takes place in the direction in which the force acts

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17
Q

What’s Newton’s Third Law?

A

to every action there is an equal and opposite reaction

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18
Q

What are the gas laws?

A

1st: Boyle’s law: at a fixed temperature, increasing pressure will decrease the volume and thus increase the density

2nd: Charle’s law: at a fixed pressure, increasing the temperature will increase the volume and thus decrease the density

3rd: Pressure law: at a fixed volume, increasing temperature or pressure will increase the other factor.

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19
Q

What’s the formula when we combine these ideal gas laws together?

A

Density=P/RT

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20
Q

What’s an adverse pressure gradient?

A

An area where the airflow is moving from low to high pressure

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21
Q

What’s the anhedral?

A

The DOWNWARD angling of the wing, root to tip

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22
Q

What’s the boundary layer?

A

A layer of air next to the aircraft skin slower than the free stream air

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23
Q

What’s the camber?

A

The shaping of the airfoil to improve lift coefficient

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24
Q

What’s the chord line?

A

The line joining the front of the airfoil to the back

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25
What the coefficient of rolling moment?
Roll moment is a moment, which is a product of a force and a distance, that tends to cause a vehicle to roll, that is to rotate about its longitudinal axis
26
What's the Centre of Gravity?
The point through which the aircraft weight acts
27
What's the Centre of Pressure?
Point through which lift and drag act
28
What's the Critical alpha?
Stall angle, the angle of attack where Coefficient of lift stops increasing
29
What's the dihedral?
The upward angling of the wing, root to tip
30
What's the dihedral?
The UPWARD angling of the wing, root to tip
31
What's EHP?
Engine shaft horsepower, the power delivered by the engine to the propeller
32
What's form drag?
An element of drag due to the form or shape of an object
33
What's incidence?
The angle between the airfoil chord line and the aircraft longitudinal axis
34
What's induced drag?
Extra drag induced by the need to generate lift
35
What's intereference drag?
An element of drag due to intereference in the airflow round wing/fuselage and other junctions
36
What's the leading edge stagnation point?
The point where the airflow comes to rest at the wing leading edge
37
What's the load factor?
The lift in manoeuvre divided by lift in level flight, or weight
38
What's the longitudinal dihedral?
The difference between the wing and tail angles of incidence
39
What's the Mean Camber line?
The line joining points equidistant from the top and bottom sufaces of an airfoil
40
What's Q?
Dynamic prsesure element
41
What's R?
Reynolds number, a non-dimensional sacle factor for airflow calculations
42
What's RAF?
Relative Airflow
43
What's RAS?
Rectified Airspeed
44
What's SAR?
Specific Air Range, miles flown in still air over fuel used
45
What's the separation point?
The point where the boundary layer separates from the airfoil surface and streamline flow breaks down
46
What's the service ceiling?
The altitude at which rate of climb has fallen to 100ft/min (propeller) or 500 ft/min (jet)
47
What's SFC?
Specific Fuel consumption, fuel used over power or thrust produced
48
What's skin friction?
An element of drag due to friction in the boundary layer
49
What's the stagnation point?
The point where the airflow is brought to rest and pressure equals total head pressure
50
What's STOL?
Short Takeoff and landing
51
What's the taper ratio?
The ratio of the root chord to the tip chord
52
What's the thickness/chord ratio?
The ratio or aerofoil thicness to chord length, expressed as a percentage
53
What's the THP?
Thrust horsepower, the power delivered by a propeller
54
What's the trailing edge stagnation point?
The point where the airflow comes to rest at the wing trailing edge
55
What's the transition point?
The point where the boundary layer changes from laminar to turbulent flow
56
What's the trim drag?
The extra drag cause by the tail forces needed to trim the aircraft
57
What's the trim point?
The angle of attack where the aircraft is in trim
58
What's V1?
Take-off decision speed
59
What's V2?¿
Take-off safety speed
60
What's Vsw?
The speed at which the onset of the natural or artificial stall warning occurs
61
What's Vx?
Best angle of climb IAS
62
What's Vy?
Best rate of climb IAS
63
What's the wash in?
Increase in incidence at the wing tip
64
What's the washout?
Reduction in incidence at the wing tip, makes the wing root stall sooner than the wingtip