Exam Flashcards

(35 cards)

1
Q

Definition of a straight line representation of a velocity

A

Length is proportional to speed using a fixed scale.

Direction is determined

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2
Q

Definition of Energy of a body

A

Capacity to do work

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3
Q

Kinetic energy definition

A

The energy a body possesses by virtue of its motion proportional to velocity KE = 1/2mv^2

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4
Q

Potential energy definition

A

The energy a body possesses by virtue of its position in a Force field = energy stored

PE =mgh

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5
Q

Gas definition

A

A group of molecules that aren’t bonded

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6
Q

Gas density

A

The measure of the number of particles per volume

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7
Q

Density of gas is a function of :

A

Temperature

Pressure

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8
Q

Camber definition

A

Max distance between the chord line and the mean camber line
Measured perpendicular to the chord line
%

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9
Q

Chord line definition

A

A straight line joining the centres of curvature of the leading edge and trailing edges

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10
Q

Relative air flow definition

A

The relative direction and speed of the air before it is influenced by the presence of the aircraft

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11
Q

Stall definition

A

AoA exceeds critical angle

Decrease in lift due to decreased pressure on top of wing

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12
Q

Thrust definition

A

Engine generates power and the propellor generates thrust by accelerating a mass of air

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13
Q

Temperature increases

A

Decrease density of gas

Increase kinetic energy

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14
Q

As pressure increases

A

Increase density of gas

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15
Q

What is static stability

A

Immediate reaction of a body disturbed by an external force

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16
Q

What is dynamic stability

A

Subsequent reaction of a body disturbed by an external force

17
Q

Symptoms of the stall

A
High attitude 
Reducing airspeed 
Stall warning 
Less effective controls 
Buffet 
Stall followed by uncommanded pitch down
18
Q

Stall recovery is

A

Reduce AoA

Increase velocity

19
Q

What are two types of drag

A

Zero lift drag

Lift dependent / induced drag

20
Q

Specific fuel consumption definition

A

Amount of fuel burnt divided by the amount of fuel produced

Jets - SFC = FF/Thrust
Turboprop - SFC = FF/SHP

21
Q

TOR(R)

A

Take off run required

Length of ground roll aircraft requires to accelerate from a standing start to speed to fly

22
Q

TORA

A

Take off runway available

Length of runway available for the ground run of an aircraft taking off

23
Q

TOD(R)

A

Take off distance required

Distance required for an aircraft to accelerate from a standing start and climb to a screen height

24
Q

TODA

A

Take off distance available

Distance available for an aircraft to achieve screen height
Includes TORA + stop way + clear way

25
ASDA
Accelerate stop distance available TORA + any stopway
26
What factors increase take off distance
``` Weight Pressure altitude Tailwind Temperature Surface Slope ```
27
Climb gradient
Distance travelled vertically divided by distance covered across the ground
28
What factors need to be considered when calculating landing performance for an aircraft
``` Aircraft weight Airfield altitude Air temperature Runway surface conditions Runway slope 50% HW 150% TW ```
29
Effects of engine failure
``` Safety implications Alters specific air range and specific ground range Decrease airspeed Decrease operating ceiling Decrease performance ```
30
Asymmetric flight
50% power lost 80% performance lost Steady flight achieved: - engine shut down and feather - gear and flap retract - 5 degree bank toward live engine - limitation of bank angle
31
Ice formation on aerofoil surfaces and fuselage
Increase thrust required and stall speed
32
Frost on wings and tail surface
Take off run and stalling speed increase
33
Not clearing frost from wings before flight
Indicated stalling speed increases
34
Accumulating clear ice on aeroplane in flight
Increase stalling speed
35
Rime ice hazard
May block pitot tube