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Module 8 Set 6

Module 8 Set 6

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practice test dgca module exam

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Module 8 set-6

Module 8 Set 6

1 / 10

WHEN THE CONTROLS ARE INCORPORATED ______________- WILL BE ACTIVATED.

2 / 10

THE POINT AT WHICH LAMINAR FLOW IS CHANGED TO TURBULENT IS

3 / 10

THE INCREASE IN ANGLE OF INCIDENCE FROM ROOT TO TIP

4 / 10

AS THE AOA OF AN AIRFOIL INCREASES THE C OF P

5 / 10

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

6 / 10

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

7 / 10

SWEEPBACK OF THE WINGS WILL

8 / 10

THE WING SETTING ANGLE IS COMMONLY KNOWN AS

9 / 10

THE C OF P IS

10 / 10

THE BOUNDARY LAYERR IS

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