Aerodynamics Flashcards

(27 cards)

1
Q

What is the relationship of lift, drag, thrust and weight when the airplane is in straight-and-level unaccelerated flight?

A

Lift equals weight, and thrust equals drag

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2
Q

Airplanes climb because of

A

Excess thrust

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3
Q

The minimum forward speed of an airplane is called the _______ speed.

A

stall

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3
Q

You can determine the proper climb altitude for your airplane by referring to the

A

airspeed indicator

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3
Q

The chord line is used to represent

A

The general shape of the wing

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3
Q

Relative wind results from the motion of the

A

airplane through the air

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3
Q

relative wind is called relative because it

A

results from the motion of the airplane

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3
Q

Relative wind is ______ and _____ to the airplanes motion

A

opposite to, equal

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4
Q

Relative wind is _____ which way the airplanes nose is pointed

A

independent of

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5
Q

An important principle to understand when dealing with angle of attack is that the nose (therefore the wing) can be pointed on an incline thats _____ the actual climb path

A

different from

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6
Q

Bernoulli figured out that the faster the air flows over a surface, the ________ pressure it exerts on that surface.

A

less

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7
Q

Air flowing faster over a curved surface causes a slight _______ in pressure on that surface

A

decrease

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8
Q

Raising the nose slightly increases the angle of attack which forces the air to undergo an additional________ greater than that which the _________ of the airfoil can produce

A

curve, engineered shape

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9
Q

An increased angle of attack permits the airplane to produce the necessary lift for flight at a ___________ airspeed

A

slower

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10
Q

When the weight of an airplane is increased, the airplane stalls at __________ indicated speed

A

higher

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11
Q

the critical angle of attack at which the wing stalls _______

A

Never changes, regardless of airplane weight

12
Q

in what flight condition must an aircraft be placed in order to spin

13
Q

during a spin to the left, which wings is are stalled

A

both wings are stalled

14
Q

wings are designed to deflect air _________ while offering very little _________ resistance.

A

vertically, horizontal

15
Q

As airspeed doubles, parasite drag ________

16
Q

as the airplane speeds up, induced drag ________ while parasite drag _____

A

decreases, increases

17
Q

wingtip vortex action increases with an increase in

A

angle of attack

18
Q

ground effect results from a/an _________ in induced drag

19
Q

as the airplane becomes airborne and flies out of ground effect, the wings downwash ______

20
Lowering flaps lowers the trailing edge of the wing, ___________ the angle the chord line makes with the relative wind. This increases the wing's lift
increasing
21
what is one purpose of wing flaps
to enable the pilot to make steeper approaches to a landing without increasing the airspeed
22
what is ground effect
the result of the interference of the surface of the earth with the airflow patterns about an airplane