Chapter 3 Flashcards

1
Q

DEFINE the boundary layer

A

The thin layer of air over an airfoil where streamlines demonstrate local airflow retardation due to viscosity

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2
Q

DESCRIBE the different types of flow within the boundary layer

A
  • Laminar flow
    • Moves smoothly along in streamlines.
    • Produces very little friction
    • Easily separated from the surface, allowing easy boundary layer separation.
    • think laminate
  • Turbulent flow
    • disorganized and irregular
    • produces large amounts of friction drag
    • adheres to surface and delays boundry layer seperation
    • raining cats that are hitting the wing, rolling, but clawing to stay on to surface
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3
Q

DESCRIBE boundary layer separation

A
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4
Q

DEFINE CL MAX AOA

A

df

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5
Q

DEFINE stall

A

fdf

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6
Q

EXPLAIN how a stall occurs

A

fddf

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7
Q

IDENTIFY the aerodynamic parameters causing a stall

A

fdf

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8
Q

COMPARE power-on and power-off stalls

A

fdf\

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9
Q

DESCRIBE the order of losing control effectiveness approaching a stall in the T-6B

A

fdf

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10
Q

EXPLAIN the difference between true and indicated stall speed

A

cvcv

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11
Q

EXPLAIN the effects of gross weight, altitude, load factor and maneuvering on stall speed, given the stall speed equation

A

sff

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12
Q

STATE the purpose of using high lift devices

A

fd

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13
Q

DESCRIBE how different high lift devices affect the values of CL, CL MAX, and CL MAX AOA

A

dfdf

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14
Q

DESCRIBE devices used to control boundary layer separation

A

fd

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15
Q

DESCRIBE devices used to change the camber of an airfoil

A

fddf

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16
Q

DESCRIBE methods of stall warning used in the T-6B

A

GFG

17
Q

DESCRIBE the stall tendency of the general types of wing planforms

A

fdf

18
Q

DESCRIBE the various methods of wing tailoring, including geometric twist, aerodynamic twist, stall strips, and stall fences

A

dfdf