Module 8 quiz contains 72 question based on the syllabus for module 5 examination for B2 category.
The time limit for the quiz is 90 min.
The number of attempts allowed are unlimited.
All the best.
Name
1.
With increasing altitude pressure decreases and
2.
The stagnation point on an aerofoil is the point where
4.
The camber of an aerofoil section is
6.
Which statement concerning heat and/or temperature is true?
7.
For a given angle of attack, induced drag is
8.
"A decrease in incidence toward the wing tip may be provided to"
10.
The relationship between induced drag and airspeed is, induced drag is
11.
The optimum angle of attack of an aerofoil is the angle at which
14.
In straight and level flight, the angle of attack of a swept wing is
16.
Above 65,800 ft temperature
17.
A decrease in pressure over the upper surface of a wing or aerofoil is responsible for
