11.1.2 Flashcards

high speed flight

1
Q

how may times is the speed of sound in water than air

A

4.3

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

4 speed ranges

A

subsonic , transonic , supersonic, hypersonic

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

subsonic speed range

A

up to 0.8

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

supersonic speed range

A

1.2-5

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

transonic speed range

A

0.8-1.2

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

hypersonic speed range

A

above mach 5

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

what property of air changes with the onset of transonic flight

A

air becomes compressible

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

what is mach number

A

aircraft speed / speed of sound

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

what is crit mach number

A

fastest speed aircraft can go without becoming subject to supersonic airflow

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

what wing design delays onset of crit mach

A

Swept wing

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

where does supersonic airflow first occur on an aerofoil

A

upper surface

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

what forms on upper surface when crit mach is reached

A

shockwave

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

what happens to airflow behind a shockwave

A

large increase in static pressure & flow separation

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

what do u oblique shockwaves do

A

slow supersonic airflow before shockwave occurs

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

where are oblique shockwaves employed

A

in the intakes

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

what happens to air velocity in an expansion wave

A

It increases

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
17
Q

why does flow separation occur behind a shockwave

A

boundary layer does not have enough kinetic energy to withstand the large increase in static pressure

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
18
Q

when does a bow wave form

A

flight speed exceeds speed of sound

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
19
Q

which wing profile is known as wing loaded

A

Transonic

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
20
Q

advantages of rear loaded profile

A

lighter, greater fuel capacity, less drag, less sweepback, smaller wing, better low speed charactericts

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
21
Q

how is tuck under avoided

A

mach trim system

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
22
Q

what drag increases due to vortex generators

A

Parasitic Drag

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
23
Q

method of reducing wave drag

A

area rule

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
24
Q

where does shockwave first form on wing

A

wing root

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
25
two types of shockwaves
normal and oblique
26
what shockwave causes an increase in velocity in airflow
none, only expansion wave causes increase in velocity
27
how does vortex generator re-energise the boundary layer
transfers energy from free airflow to the boundary layer
28
when does the boundary layer separate from aerofoil section
when the normal shockwave forms
29
what effect does aerodynamic heating have on metal
they lose strength
30
what point is airflow over a wing at its maximum but below speed of sound
Critical mach number
31
normal swept wing angle
30 degrees
32
transonic wing profile
flatter upper surface curved leading edge thinner trailing edge than normal
33
how is shock stall corrected
with horizontal stabiliser
34
where is c.o.g located on balance control surface
on hinge line
35
how is high speed turn controlled by flying control surfaces
aileron and roll spoilers
36
what automatic system of the horizontal stabiliser corrects tuck under
Mach trim
37
how many ailerons fitted to large aircraft
4 , 2 outbound, 2 inbound
38
when do inbound ailerons operate
low speed and high speed
39
when do outbound ailerons operate
low speed only
40
aluminium strength lose how much strength at temperatures over 250 degrees
80%
41
On a swept wing where does it stall first
Tip
42
Dutch roll is movement is in which direction
Yaw and roll
43
What are Kruger flaps
Leading edge flap hinges
44
How are peto tubes heated
Electrically
45
What is the artificial feel system used for
Required for power operated systems
46
Where does shockwaves form
Highest point of camber
47
when does a bow wave form
Above speed of sound
48
What does vortex generator do
Re-energises boundary layer
49
Purpose of swept wing
Aerodynamic purposes creating a longer thinner wing with an angle of 30 degrees
50
Why do transonic profiles perform well in transonic reigons
There’s no flow separation behind the shockwave as this flow would generate lift
51
If velocity increases what happens to the centre of pressure
Moves rearwards
52
How is centre of pressure moving rearward offset
By horizontal stabiliser
53
What are the waves formed by supersonic flow
Shock waves and expansion waves
54
How can we increase critical Mach
Decreasing camber and increasing chord
55
What happens during stall shock
Lift increases and drag decrees
56
What happens to crit mach with a thicker camber
Crit Mach lowers
57
How much faster is speed of sound in water than air
4.3 times out of
58
How much faster is speed of sound in air than water
4.3 times slower
59
What’s another name for flight tabs
Servo tab
60
Where is the balance panel effective
High speeds