Part III Flashcards

(36 cards)

1
Q

What is the general rule of thumb about computer time and Re when simulating

A

PU time = Re^3

Storage requirement = Re^9/4

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2
Q

What is Breguet Range cruise distance equation

A

R = V/c * L/D * ln( Winitial / Wfinal)

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3
Q

What is payload fraction

A

payload/ total lift off weight

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4
Q

Was is useful payload fraction

A

payload + fuel / MTOW

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5
Q

What is fuel fraction estimation equation

A

Wf/Wo = 1.06(1-Wx/Wo)

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6
Q

Define stability

A

ability of aircraft to return to its original equilibrium position

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7
Q

Define control

A

ability of the pilot to produce moments about the various axis

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8
Q

Define static stability

A

Refers to the tendency of the aircraft to counter a disturbance

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9
Q

Dynamic stability

A

is concerned with how fast the aircraft returns to trim condition after a disturbance

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10
Q

For cambered aerofoils, if centre of pressure moves, what happens to the pitching moment at the aerodynamic centre

A

stays the same

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11
Q

What equation represents static stability

A

x / c

where:
x - distance between CG and AC
c - chord length

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12
Q

What is a canard

A

when the tail wing is in front of the main wing

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13
Q

List 2 benefits of canards

A
  1. Canard surface operates at high CL and almost makes aircraft ‘stall-proof’
  2. Can sometimes have larger range for CG
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14
Q

List 2 disadvantages of canards

A
  1. Wing operates in downwash from canard and therefore reducing its efficiency
  2. Difficult to apply flaps to wings
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15
Q

What is a flying wing design

A

an aircraft design with no tail (lowest possible drag)

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16
Q

Benefits of a flying wing design

A
  • Removes fuselage therefore improves aerodynamic efficiency
  • synergistic effect with relaxed static stability
  • low visibility on radar
  • distribute load easier
17
Q

What is drag crisis

A

In the transition period between laminar and turbulent flow, drag drops

18
Q

What is the reason for the drag crisis

A

When turbulence rapidly mixes rapidly-moving external air into the boundary layer, increasing the range over which it adheres to the surface. This makes the trailing low pressure wake smaller and thus reduces drag

19
Q

What can be done to a surface to ensure drag crisis happen more

A

roughening the surface i.e. golf ball

20
Q

What is the wall law

A

velocity of turbulent flow ∝ log(distance to the wall)

only works when distance < 20% of flow height

21
Q

What are streaks and what happens when they meander

A

Turbulent flows vortices form near a wall and are stretched by the mean flow - these are streaks

When they meander, this causes friction and drag to increase

22
Q

equation for streak size, spacing and length

A

size = a+ = ua/v (10y)

spacing = s+ = us/v (100y)

length = l+ = ul/v (1000y)

where:
u = friction velocity at wall
y = distance to wall
v = local kinematic viscocity

23
Q

What are riblets

A

a series of parallel grooves on a surface that can reduce drag and make a wall more streamlined

they are used to channel vortex streaks created near the wall

24
Q

List advantages of open circuit tunnels

A
  1. less expensive to build

2. pollutants are purged (smoke)

25
List disadvantages of open circuit tunnels
1. more expensive to run 2. affects design of surrounding environment 3. more noisy
26
List advantages of closed circuit tunnels
1. some energy is recovered 2. shielded from weather 3. quality of flow easily controlled
27
List disadvantages of closed circuit tunnels
1. more expensive to build 2. air inside constantly heated 3. full of dust and debris 4. noisy
28
Give equation for energy ratio of wind tunnel
Jet energy / sum of circuit losses qUA / efficiency * motor power
29
How to manage turbulence in wind tunnel
via honeycomb and screens
30
What is hot wire anemometry used for
used to calculate pressure and velocity of airflow how: - heated wire - gives off heat via convection to airflow - energy required to reheat is directly proportional to airflow
31
Advantages of hot wire anemometry
1. cheap | 2. accurate
32
Disadvantages of hot wire anemometry
1. effects airflow 2. can't measure high intensity turbulence 3. wind direction has no effect 4. very fragile 5. can 'burn out'
33
What can be used to measure velocity and pressure in multi-phase situations
hot film probe | more expensive and worse frequency response then hot wire anemometry however
34
What is LDV
Laser Doppler Velocemetry | - use doppler effect to measure velocity/pressure
35
What is PIV
Particle Image velocemetry - have particles in fluid that light up under a laser - post-process images to find velocity/pressure - can create 2D/3D velocity fields
36
What equation shows that flight is stable
dCmp / dCl < 0