Drag (Chapter 7) Flashcards

1
Q

Laminar flow changes to turbulent flow at the……………point

A

Transition point

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2
Q

The transition point shall never be:

A

Aft of the maximum thickness of the aerofoil

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3
Q

Laminar air flow has a ___________ velocity gradient

A

shallow

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4
Q

Turbulent airflow has a _____________ velocity gradient

A

Steep

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5
Q

The lowest pressure of an aerofoil is on the _______ of the aerofoil

A

Top

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6
Q

The separation point shall move __________ with an increase in AoA

A

Forwards

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7
Q

Laminar flow is:

A

Low Energy
Thin layer (1-2mm)
Predictable airflow

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8
Q

Turbulent airflow is:

A

High energy
Thick layer (2-3cm)
Mixed airflow

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9
Q

Reynolds Number is:

A

A dimensionless number which states the type of airflow (<500,00 is laminar) (>10,000,000 is turbulent)

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10
Q

Skin Friction drag

A

The drag which occurs within the boundary layer of the aerofoil

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11
Q

Form Drag

A

The drag which is created due to the pressure differential behind the trailing edge of the aerofoil

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