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Module 8 Set 5

Module 8 Set 5

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Practice test for dgca module 8 exam

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Module 8 Set 5

Module 8 Set 5

1 / 20

UPWARD AND OUT WARD INCLINATION OF A MAIN PLANE  IS TERMED AS

2 / 20

WHEN AN AIRCRAFT STALLS

3 / 20

DIRECTIONAL CONTROL IS PROVIDED BY

4 / 20

WHAT IS THE ANGLE B/W THE CHORD LINE OF WING, AND THE LONGITUDINAL AXIS OF THE A/C KNOWN AS

5 / 20

THE BOUNDARY LAYERR IS

6 / 20

SWEEPBACK OF THE WINGS WILL

7 / 20

LONGITUDINAL STABILITY IS GIVEN BY

8 / 20

THE C OF P IS

9 / 20

THE WING SETTING ANGLE IS COMMONLY KNOWN AS

10 / 20

AS THE AOA OF AN AIRFOIL INCREASES THE C OF P

11 / 20

WHICH TYPE OF FLAP CHANGES THE AREA OF THE WING?

12 / 20

AILERON PROVIDE WHICH CONTROL

13 / 20

TO REDUCE TAKE OFF RUNWAY RANGE AIRCRAFT FLY

14 / 20

DENSITY OF AIR

15 / 20

THE POINT AT WHICH LAMINAR FLOW IS CHANGED TO TURBULENT IS

16 / 20

THE INCREASE IN ANGLE OF INCIDENCE FROM ROOT TO TIP

17 / 20

THE AXIS WHICH PASSES FROM NOSE TO TAIL IS CALLED

18 / 20

WHEN THE CONTROLS ARE INCORPORATED ______________- WILL BE ACTIVATED.

19 / 20

THE STRAIGHT LINE PASSES  FROM L.E OF THE WING TO THE T.E IS CALLED

20 / 20

DENSITY OF AIR AT SEA LEVEL

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