POF - Drag Flashcards

1
Q

What are the two types of drag?

A
  1. Form Drag

2. Skin-Friction Drag

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2
Q

Why is it better to have a maximum thickness near the trailing edge?

A
  1. It delays the transition point.
  2. The surface maintains a laminar flow longer.
  3. It reduces skin friction drag.
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3
Q

What is the boundary layer?

A

It is the area that extends from the surface up to the flow speed that is 99% of the free stream flow

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4
Q

What is a pressure gradient?

A

It is when pressure moves from high pressure to low pressure.

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5
Q

What does a high Reynolds number mean?

A

A high Reynolds number means turbulent flows.

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6
Q

What are three factors that affect the transition point of a boundary?

A
  1. Speed of the airflow.
  2. Surface quality.
  3. Magnitude of adverse pressure gradient.
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7
Q

What does a low Reynolds number mean?

A

A low Reynolds number means laminar flows.

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8
Q

What is form drag?

A

When there is a pressure differential on the surface of the object.

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9
Q

What is the transition point?

A

It is the point on the surface when laminar flow changes to a turbulent flow.

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10
Q

If the aerofoil is thick towards the trailing edge, where would the transition point be?

A

The transition point would be further away from the leading edge.

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11
Q

What is profile drag?

A

Profile drag is form and skin-friction drag.

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12
Q

Where is the transition point on an aerofoil that’s thick near the leading edge?

A

The transition point is closer to the leading edge.

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13
Q

What are four key facts about the laminar boundary layer?

A
  1. It has a laminar flow.
  2. It is thin (mm).
  3. Slippery
  4. Has low kinetic energy.
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14
Q

What are four key facts about the turbulent boundary layer?

A
  1. It has turbulent flows.
  2. It is thick (cm).
  3. It is draggy.
  4. Has high kinetic energy.
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15
Q

What is the formula for Drag?

A

Drag Force = 1/2•rho•V^2•S•CD

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16
Q

What is skin-friction drag?

A

When there is friction between air molecules and the upper surface of the aerofoil.

17
Q

What are two factors that affect the pressure gradient?

A
  1. It is influenced by the difference in magnitude between two pressure pockets.
  2. Distance between the two pressure pockets.
18
Q

What is the separation point?

A

When the boundary layer separates itself from the upper surface of the aerofoil.