Aeroacoustics Flashcards

1
Q

What is aerofoil self noise?

A

Noise generated by the interaction an aerofoil with its boundary layers and wake
- dominant at lower wind speeds/higher frequency

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2
Q

What is In-flow turbulence?

A

Noise caused by upstream atmospheric turbulence

- dominant at higher wind speeds/lower frequency

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3
Q

What is trailing edge noise?

A

Turbulent boundary layer interacts with trailing edge

- Minimised through design of aerofoil section at trailing edge

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4
Q

What is laminar boundary layer vortex shedding?

A

Instability in separated laminar flow from lower edge of blade

  • Minimised by preventing separation through blade design
  • Serrated leading edge effective
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5
Q

What is boundary layer separation and stall noise?

A

Separated boundary layer becomes turbulent and interacts with blade surface

  • Increases with angle of attack
  • Minimised by blade pitch regulation
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6
Q

What is trailing edge bluntness vortex shedding?

A

Instability in wake due to thickness of trailing edge

- Minimised by using a sharper blade profile

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7
Q

What is tip vortex formation?

A

Separated vortex flow interacts with blade surface

- Minimised through design of the tip shape

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8
Q

8 ways to reduce aerofoil noise

A
  • serrated aerofoils
  • porous treatment
  • morphing structures
  • surface treatment
  • flow suction
  • flow injection
  • micro jets
  • sweeping jets
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9
Q

Pros and Cons of Surface treatment to reduce noise?

A

+ very effective in controlling noise
+ minimum impact on aerodynamic performance
- Involves very complex flow physics

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10
Q

Where is future research focused for surface treatment?

A
  • better understanding of flow physics and noise control mechanism
  • more novel/effective treatment
  • application to other aeroacoustic applications
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11
Q

When is FWH (Ffowcs Williams–Hawkings) used?

A

Aeroacoustic sources in relative motion with respect to a hard surface

Turbulence is moving

Two distinct regions of fluid flow

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12
Q

What are free space Green’s functions?

A

Adds a volume source to the continuity equation

Adds an external force to the momentum

Combined to form a ‘forced’ wave equation

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13
Q

What do monopoles, dipoles and quadrupoles look like in the context of the FWH integral

A

Monopiles have no spatial derivatives (only a temporal)

Dipoles have one spatial derivative (x_i)

Quadrupoles have two spatial derivatives (x_i and x_j)

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