Pilot class-006- Lift and Weight

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Created on April 07, 2020 By

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Quiz-006

1 / 8

the aerodynamic force of weight on an aircraft is the effect of:

Gravity

Lift

Drag

2 / 8

Lift is counteracted by

Weight

Thrust

Drag

3 / 8

To create lift in a symmetrical aerofoil

Angle of Attack has to be decreased

Angle of Incidence has to be increased

Angle of Attack has to be increased

4 / 8

Lift is caused because of

Airflow

Pressure differential

Angle of incidence

5 / 8

At the stagnation point

Airflow has zero velocity

Airflow is accumulated

Airflow has max velocity

6 / 8

The most desirable airflow flying is

Turbulent airflow

Laminar Airflow

Relative Airflow

7 / 8

Angle of Incidence is the angle between

Chord and mean camber line

Chord and longitudinal axis of Aircraft

chord and relative airflow

8 / 8

Angle of Attack is the angle between

Chord and relative airflow

Chord and longitudinal axis of Aircraft

Chord and mean camber line

Your score is

The average score is 77%

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