Lift Flashcards

1
Q

The equation of continuity states that?

A

Mass can neither be created nor destroyed

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2
Q

The result of the equation of continuity is?

A

Air mass flow is a constant

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3
Q

Bernoulli’s theorem states that?

A

in the streamline flow of an ideal fluid, the sum of the potential energy plus the pressure energy plus the kinetic energy will remain constant.

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4
Q

Considering Bernoulli’s theorem, if kinetic energy increases what will be the effect of pressure energy?

A

Since the sum of energy needs to remain constant, if kinetic energy increase pressure energy decreases.

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5
Q

The rearranged kinetic energy formula =

A

1/2 p v^2

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6
Q

The fineness ratio is?

A

The ratio of depth to length of a streamlined body

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7
Q

Define the lift formula, and the individual meanings.

A

CL 1/2 P V^2 S

CL is the coefficient of lift, which is the value of lift for a given angle of attack

1/2 RHO is the air density

V^2 is the velocity(TAS) in feet or metres per second squared. In other words, if the speed is doubled, the lift increases fourfold

S is the surface area

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8
Q

The centre of pressure moves forward with an increase in angle of attack due to?

A

The effective thickness of the aerofoil increasing

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9
Q

A faster wing will have what type of thickness/chord ratio?

A

A low ratio

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10
Q

Over the top surface of an aerofoil the flow begins to slow down at -

And is called?

A

or slightly behind the point of maximum camber.

The transition point

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11
Q

The point where the airflow changes from laminar to turbulent is called?

A

The transition point

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12
Q

The definition of wing span is?

A

The length from wing tip to wing tip

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