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Module:     Show:
Module 13. Aircraft aerodynamics, structures and systems
When approaching the speed of s
•  pressure above the wing the wing in places
•  pressure above the wing equals the pressure below the wing
•  pressure above the wing can never exceed the pressure below the wing

Dusiata asking:
•  Can somebody place full question and answer? Should it be "speed of sound"?

Community comments: 0
Module 13. Aircraft aerodynamics, structures and systems
The ATC aerial has a polar diagram which is
•  directional
•  omni-dirrectional
•  limacon shaped

Dusiata asking:
•  Directional? Maybe they have in mind radar antenna?

Community comments: 0
Module 13. Aircraft aerodynamics, structures and systems
With a bonding meter
•  it does not matter which lead goes where
•  the short lead to the aircraft airframe and long lead to the item
•  the long lead is attached to the aircraft air frame and short lead to item

Dusiata asking:
•  Could you show which lead is longer on most common T477W bonding meter? I hope there won't be such questions on real exam...

Community comments: 0
Module 13. Aircraft aerodynamics, structures and systems
Mode C response is
•  8 microseconds
•  12 microseconds
•  21microseconds

avionics asking:
•  I think it should be 21microsec p1 n p3 respond

Community comments: 0
Module 8. Basic aerodynamics
With increasing altitude the angle at which a wing will stall
•  remains the same.
•  reduces.
•  increases.

pB1B2 asking:
•  why?


Community comments: 2
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