Intro Flashcards

1
Q

What do you times m/s by to get knots?

A

1.944

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2
Q

What is the equation of continuity

A

Conservation of mass flow

As area goes down velocity must go up keep the same volume of air traveling through a gap

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3
Q

What phenomena makes air “hug” the top edge of an aero foil

A

The Coanda effect

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4
Q

What is Bernoulli’s theorem

A

That as dynamic pressure increases static pressure must decrease and the same for the reverse

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5
Q

What is form drag

A

The difference in pressure from front to back of an object

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6
Q

Where is the centre of pressure on a aerofoil

A

25% of the aerofoil from the front

Cambered aerofoil = 23.5-27%

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7
Q

Why is there a drop in static pressure above the wing

A

As air goes over the leading edge radius it’s speed (dynamic pressure) increases therefor static pressure decreases

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8
Q

What is the thickness - chord ratio

A

Ratio between aerofoils max thickness to its length

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9
Q

What does total reaction depend on

A

Coefficient of life and the dynamic pressure

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10
Q

With a symmetrical wing what happens when AOA is increases

A

Cal increases linearly

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11
Q

What happens as thickness is increased of a aerofoil

A

Cl max increases

Stalling angle of attack increases

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12
Q

What are the effects of camber on an aerofoil

A

Higher cl max

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13
Q

What are the effects of training edge flaps

A

= increases camber = increased lift

Lower stall angle of attack

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