Airplane Design Flashcards

1
Q

An airplanes’ location of it’s CG (center of gravity-in front of wings) and CL (center of lift- at wings), determines its’ ________________ stability.

A

Longitudinal

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2
Q

As an airplanes’ CG moves aft, the plane becomes….

A

Less stable

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3
Q

To minimize side loads played on an airplane’s tricycle landing gear during touchdown, the pilot should

A

Keep the longitudinal body of the plane parallel with its direction of movement

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4
Q

Primary flight controls become (more/less) stable as airspeed (increases/decreases).

A

More as increases
-this is because there is more air moving over the control surfaces

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5
Q

Flaps allow pilots to…

A

Make steeper approaches without increasing airspeed

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6
Q

An airplane has been loaded in such a manner that the CG is located aft of the CG limit. One undesirable flight characteristic a pilot might experience would be…

A

Difficulty recovering from a stall

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7
Q

Longitudinal stability refers to an aircraft’s stability about which axis?

A

Lateral

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8
Q

An airplane that is more stable will….

A

Require less effort to control

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9
Q

Center of pressure is the same as….

A

Center of lift (at wings)

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10
Q

Changes in the center of pressure of a wing affect the aircraft’s…

A

aerodynamic balance and controllability

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11
Q

Purpose of rudder is to….

A

Control yaw

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12
Q

Loading an airplane the most aft CG will cause….

A

The plane to be unstable at all airspeeds

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13
Q

3 Types of Single Engine Aircraft that require a special endorsement to fly

A

High performance
-201+ hp

Complex
-retractable landing gear, controllable propeller, flaps

Tailwheel
-Conventional landing gear with wheel on tail

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14
Q

When does lift equal weight and thrust equal drag?

A

In unaccelerated flight

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15
Q

Bernouilli’s Principle states that when the speed of a fluid _________ it’s pressure _________. This also refers to an airplanes’ ___________.

A

Increases
Decreases

Wing
This causes air molecules to create a low pressure above the wing because they are hitting the leading edge of the wing, thus speeding up. Below the wing is still moving the same speed so it is a higher pressure. Air molecules want to move from high to low so lift is produced.

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16
Q

Angle of attack is defined as:

A

Angle between the chord line of the airfoil (wing) and the relative wind.

17
Q

Ailerons control movement about which axis?

A

Longitudinal
(Roll)

18
Q

Rudder control movement about which axis?

A

Vertical
(Yaw)

19
Q

Elevator controls movement about which axis?

A

Lateral
(Angle of Attack)

20
Q

Newton’s third law states in relationship to an airplane….

A

For every motion there is an opposite and equal reaction.

An additional upward force is created on the bottom of a wing as air hits and is deflected downward.

21
Q

When do we have left turning tendencies in the airplane?

A

When climbing out. Need right rudder to correct.

22
Q

When do we have right turning tendencies?

A

In a climb, need right rudder.

23
Q

4 Left Turning Tendency Factors

A

Gyroscopic Procession- prop spins right causing a shift to the left
P-Factor- prop spins right, blade is scooping harder on the down spin than on up spin causing more thrust on the right, pushing plane left due to asymmetrical thrust
Torque- prop spins right, causes tail and fuselage to torque left
Spiraling Slipstream- air spins behind prop around the fuselage, striking left side of the tail causing it to turn the plane left

24
Q

Why do we have canted wings (sloped upward towards the tips)?

A

Dihedral lines
-When we dip for a turn, more lift is produced on uplifted wing
-dihedral line becomes more horizontal as we turn, resulting in more lift on that wing

25
Q

Explain Keel Effect

A

If wings are the water, a high winged aircraft has most of the plane below the “water”.
-plane acts as a keel to steady and keep plane from overly slipping and skidding

Low wing planes do not have this present and must input stronger rudder control

26
Q

Purpose of horizontal stabilizers

A

Sloped down in the front
Catch air eddying from wings
Creates pressure differential causing downward force to offset weight of front engine