A103 Aerodynamics Flashcards

1
Q

Where is the center of gravity?

A

Origin for lateral (pitch), lognitudinal (roll), and vertical (yaw) axis

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2
Q

What is the angle of attack?

A

The angle between the relative wind and the chord line

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3
Q

What causes a stall?

A

When the critical angle of attack is exceeded, and lift can no longer be generated

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4
Q

What causes lift?

A
  • Bernoulli’s Principle increased velocity over the curved upper side of the wing causes increased velocity and low pressure, lower velocity higher pressure air flows under the wing
  • Newton’s Third law
    As air is deflected downward by the wing the wing is deflected upward
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5
Q

What are the types of Parasitic Drag

A
  • Form drag
  • Interference drag
  • Skin friction drag
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6
Q

What is form drag?

A
  • Parasite drag from turbulent wake caused by airflow around a structure
  • Depends on size and shape of structure
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7
Q

What is Interference Drag?

A
  • Parasite drag from interaction of varied currents that flow over an airplane and mix together
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8
Q

What is Skin Friction Drag?

A
  • Parasite drag from roughness of airplane
    surfaces
  • Rivet heads
  • Irregularities (bugs / dirt)
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9
Q

What is Induced Drag?

A
  • Drag created by the
    production of lift
  • Inversely proportional
    to square of the speed * Half airspeed = Four
    times induced drag
  • Predominant at low
    airspeeds (high AOA)
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10
Q

What causes turning flight?

A
  • Horizontal component of lift
    causes airplane to turn
  • When vertical component of
    lift equals weight aircraft will
    neither gain nor lose altitude
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11
Q

What is ground effect, when is it strongest, and are high or low wing planes affected more?

A
  • Phenomenon of less induced drag close to ground
  • Earth’s surface alters airflow patterns around aircraft
    reducing downward deflection of airstream
  • At height equal to wingspan and lower
  • More noticeable on low wing aircraft as wing gets close to
    ground during takeoff and landing
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12
Q

What is critical angle of attack?

A

The point where the coefficient of lift is maximum is CL Max

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13
Q

What causes a spin?

A
  • Combination of Stall & Yaw
  • Uncoordinated stall resulting in a descending
    corkscrew path
  • One wing more stalled than other
  • Will spin in same direction as yaw
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14
Q

What is adverse yaw and how do we account for it?

A
  • While rolling into a turn, outside wing produces more lift
  • Induced drag increases on outside wing
  • The increased induced drag causes yaw opposite of the direction of the roll
  • Use rudder in the direction of the roll in coordination with ailerons to compensate for adverse yaw
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15
Q

What is load factor?

A

Ratio of:
Load supported by the wings
to
Actual weight of the aircraft and contents

Increasing load factor will
cause an airplane to stall at
a higher speed

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16
Q

What are the four turning tendancies?

A
  • Torque (L)
  • Gyroscopic precession (R)
  • Asymmetrical thrust or P-Factor (L)
  • Spiraling slipstream (L)

Note: These are most often noticeable at high power settings & low
airspeed situations.

17
Q

Explain the torque turning tendency

A
  • Newton – “For every action there is an equal and
    opposite reaction”
  • Propeller rotates clockwise – causes torque which
    tends to rotate airplane counterclockwise about
    longitudinal axis
    ** LEFT **
18
Q

Explain the Gyroscopic Precession turning tendency

A
  • Precession is resultant reaction when force applied to rim of rotating disk
  • In a nose gear aircraft, tendency on takeoff and landing flare is a yaw to the right due to propeller
19
Q

Explain the Asymmetrical Thrust (P-factor) turning tendency

A
  • Airplane flown at high power and high angle of attack
  • Uneven angles of attack between ascending left side and descending right side blades
  • Unequal thrust causes yaw to left (bigger “bite” of air on right side)
20
Q

Explain the Spiraling Slipstream turning tendency

A
  • Slipstream from
    propeller wraps around
    fuselage and hits left
    side of vertical fin
  • Causes tail to move
    right – nose to yaw left
21
Q

What are the 3 stages of a spin?

A

Incipient
Developed
Recovery