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Dgca Module 08 Online Test Quiz! 60

Dgca Module 08 Online Test Quiz! 60

Dgca Module 08 Online Test Quiz!

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Quiz Questions And Answers

Reynolds number

Is applicable to supersonic aircraft
Is applicable to continuous flow
Both a and b

The optimum angle of attack of an aerofoil is the angle at which:

The aerofoil produces maximum lift
The aerofoil produces zero lift
The highest lift/drag ratio is produced

In steeper turn rudder position is taken by:

Elevator
Rudder
Aileron

The angle between the main plane and tail plane is known as?

Angle of attack
Angle of bank
Longitudinal Dihedral angle

Atmospheric pressure measured with an instrument called

Altimeter
Anemometer
Barometer

Higher Reynolds number.

Supersonic -turbojet engine
Subsonic -aircrafts
None of the above

During climbing turn lift on an inner wing is

More
Same
Less

Longitudinal stability is affected by:

Wing
Fuselage
Hull

During equilibrium flight operation stability depends on:

Magnitude of X force applied
Length from the C.G
Both a and b

During takeoff preferably aircraft will go:

Against the wind
Along with wind
None of the above
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