Aerodynamics Lesson 2

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Last updated 3:37 AM on 2/6/26
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46 Terms

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Physical Description of Lift

a wing produces lift by diverting air down

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How do wings develop lift?

by diverting air down

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Most of the lift is…

due to the action over the top of the wing

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<p>A wing that is creating no lift</p>

A wing that is creating no lift

Since no air was deflected downward, there is no net action on the air, which means there was no reaction on the wing

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<p>Downwash </p>

Downwash

The downward traveling air around the wing; the action that causes the reaction of lift

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<p>What is occurring since there has been a net change in the air passing over the wing?</p>

What is occurring since there has been a net change in the air passing over the wing?

There is a force acting on the air and a reaction force acting on the wing

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How a wing generates lift in one sentence:

The wing produces lift by diverting air down.

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Coanda Effect

A phenomenon that explains why fluids follow the shape of curved surfaces

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<p>The direction of the force on the air is perpendicular to…</p>

The direction of the force on the air is perpendicular to…

the bend and the magnitude (size) of the force is proportional to the tightness of the bend

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<p>What do these forces, working through pressure, represent?</p>

What do these forces, working through pressure, represent?

the mechanism in which the force is transferred to the wing

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Forces on a Wing Applying to Newton:
How is downwash produced?

Air bends around the wing

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Forces on a Wing Applying to Newton:
How does this apply to Newton’s first law?

bending the air requires a force on the air

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Forces on a Wing Applying to Newton:
How does this apply to Newton’s third law?

There is an equal and opposite force on the wing

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Forces on a Wing Applying to Newton:
The pressure difference across the wing is the mechanism…

by which lift is transferred to the wing owing to the bending of the air

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Newton’s Second Law:

Lift is proportional to the

amount of air diverted per time multiplied by the vertical velocity of that air

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How can the lift of a wing be increased?

by increasing the amount of air diverted, the vertical velocity of that air, or a combination of the two

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What happens to lift when we double speed?

Vertical velocity will double, but also the amount of air diverted per unit of time will double.

This means that the lift of the wing has gone up by a factor of 4

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What if you double the angle of attack but speed stays the same?

The vertical velocity will double but the amount of air diverted is unaffected so lift on the wing doubles.

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traditional definition of Geometric Angle of Attack

Angle between the chord line of the wing and the relative wind.

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Effective Angle of Attack

Angle measured from the orientation where the wing has zero lift.

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Critical Angle of Attack

The point where the angle of attack becomes so great that the airflow begins to separate from the trailing edge of the wing. This is where the stall begins.

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Vertical velocity is proportional to?

the speed of the wing and the effective angle of attack of the wing

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The amount of air being moved changes based on what?

air density and the speed of the aircraft

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Where is more air diverted on a wing?

near the wing root rather than the wing tip

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Drag

the retarding force that opposes an aircraft's motion through the air, requiring a certain amount of thrust to fly at a constant speed

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Induced Drag

a byproduct of lift that increases as the angle of attack increases

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What type of drag is always present as long as there is lift being generated?

Induced Drag

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How does parasite drag increase?

It increases with the aircraft’s speed

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The three types of Parasite Drag

Form Drag

Skin-Friction Drag

Interference Drag

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Form Drag

created due to the shape of the aircraft and its protrusions

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Skin-Friction Drag

A result of the aircraft’s surface being rough and can be viewed all the way to the microscopic level

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Interference Drag

Occurs when two different airflows meet, mix, speed up, and become turbulent. This meeting of airflows increases energy loss.

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_______ on the SR-20 help to reduce the effects of ________ _________

Fairings; Interference drag

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Power

The rate at which work is done. In regard to an aircraft that has an engine, we can think of ______ as the rate fuel is consumed

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<p>This graph shows the amount of power required to overcome drag and? </p>

This graph shows the amount of power required to overcome drag and?

maintain a constant speed and altitude

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<p>What is more prevalent at slower speeds? </p>

What is more prevalent at slower speeds?

Induced drag

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<p>As <u>speed</u> increases, ______  _______ decreases and _________  _____ increases to where more power is required to overcome those effects  </p>

As speed increases, ______ _______ decreases and _________ _____ increases to where more power is required to overcome those effects

induced drag; parasitic drag

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The point on the power curve where the effects of induced drag and parasitic drag (total drag) are minimized

L/D Max

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Effects of Altitude on Power Required:
(This is why it is harder to breathe at high altitudes)

With an increase in altitude, there is a decrease in air density.

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What must be increased as what is decreased to produce enough lift?

The angle of attack; air density

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<p>What happens to the <strong>downwash</strong> if you <strong>double the weight of an aircraft</strong> but want to maintain the <strong>same airspeed</strong>?</p>

What happens to the downwash if you double the weight of an aircraft but want to maintain the same airspeed?

The vertical velocity of the downwash must double.

  • This is because the rate (mass) of air diverted stays the same, so to generate twice the lift (for double the weight), each unit of air must be deflected twice as fast downward.

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Aspect ratio formula

wing span² / wing area

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What happens to a wing’s efficiency when it flies close to the ground?

It experiences an increase in efficiency (reduced induced drag) when flying within about 1 wing’s length of the ground — this is known as ground effect.

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Because of the additional lift under the wing created when in ground effect, what can be reduced, and how does this affect the angle of the downwash and induced drag?

Because of the additional lift under the wing, the angle of attack can be reduced, which reduces the angle of the downwash and decreases induced drag.

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Problems with Bernoulli

Equilibrium means that no energy can be added to or removed from the airflow.

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Problems With Bernoulli

In order to oppose the induced drag caused by lift, external work must be done by the
engine or else the wing will decelerate, which means it is not in equilibrium.