Aerodynamics Flashcards

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

A

stalled

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 ________

A

quadruples

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

A

decrease

19
Q

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

A

increases

20
Q

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

A

increasing

21
Q

what is one purpose of wing flaps

A

to enable the pilot to make steeper approaches to a landing without increasing the airspeed

22
Q

what is ground effect

A

the result of the interference of the surface of the earth with the airflow patterns about an airplane