Aerodynamics Flashcards

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1
Q

Bernoulli’s Principle

A

Increased speed equals lower pressure. Lower pressure on the airfoil higher pressure on the lower portion of the wing. Venturi principle. High Pressure pushes low pressure up

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2
Q

Chord line

A

line through the middle of the aircraft wing

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3
Q

Upper surface camber and lower surface camber

A

top and bottom of the wing, and the mean camber runs in between the perfectly or equal distance… flaps increase camber line.

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4
Q

Leading edge vs tailing edge

A

front of the wing, back of the wing

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5
Q

angle of attack

A

angle between the chord line and relative wind

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6
Q

Critical Angle of Attack

A

the point at which a plane can stall

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7
Q

Relative Wind

A

Runs parallel and opposite of the wings path

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8
Q

Why does air accelerate on the top of a wing?

A

The Coanda affect

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9
Q

As we increase angle of attack we get what?

A

Wind deflection down from the lower surface camber and pushes the plane up

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10
Q

What affect do wing tip vortices have on our plane

A

Induces drag

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11
Q

Wake Turbulence is strongest when the plane is what?

A

Heavy clean and slow

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12
Q

Equation for lift

A

LIft= coefficient of lift x pressure(Density) x velocity squared x surface area divided by two

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13
Q

What are the two types of drag?

A

Induced and Parasitic

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14
Q

What is parasitic drag?

A
  1. Form- designed into the airplane, the least time it takes for the air to move from the front to the back of the aircraft the better
  2. Interference: different airflows that intersect. Anything at a 90 deg angle on the plane causes interference drag
  3. Skin Friction: all surfaces have an imperfectly smooth surface. Fluid air running into that induces drag
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15
Q

Maneuverability

A

the aircrafts ability to maneuver and not break

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16
Q

Controllability

A

The reaction your plane has to your inputs

17
Q

What are the two types of Stability?

A

Static stability is the initial tendency

Dynamic Stability how it reacts over time

18
Q

Static Stability: What is positive, neutral, and negative stability?

A

Positive returns, negative gets worse, neutral remains the same

19
Q

Vertical axis

A

controls yaw, rudder

20
Q

Longitudinal Axis

A

length of plane, controls bank, ailerons

21
Q

Lateral Axis

A

pitch, stabilator, wings

22
Q

Center of lift is normally aft or infront of CG

A

aft of CG

23
Q

How does moving the CG affect our performance

A

if the cg is too far forward it affects several aspects of performance

Cruise Performance: decreased with a forward CG
Stall Speed: Increases
Stall Recovery: Better
Take off performance: Longer ground roll, not a great climb
Landing performance: trouble rounding out or flaring
Stability: better

24
Q

Aft CG affects

A

Cruise performance: better
Stall Speed: lowers
Stall recovery: worse
Take off performance: Worse, tail strike possibilities.
Landing performance: trouble round out flare
Stability: Better

25
Q

Dihedral

A

make the plane more stable

26
Q

Our planes have what type of ailerons?

A

differential ailerons. goes up 25 degrees, the other goes down 12.5 degrees. allows for less rudder inputs in the left turn

27
Q

what turns a plane?

A

The horizontal component of lift