Quiz ATPL | Page 31 | Principles of Flight

The lift coefficient (CL) of an aeroplane in steady horizontal flight is 0.35. An increase in angle of attack of 1 degree would increase CL by 0.079. If a vertical gust instantly changes the angle of attack by 2 degrees, the load factor will be:	4 risposte
Which definition of propeller parameters is correct?	4 risposte
In twin-engine aeroplanes with right turning propellers	4 risposte
Which one of the following statements about Bernoulli's theorem is correct?	4 risposte
The unit of density is:	4 risposte
The angle of attack of a wing profile is defined as the angle between:	4 risposte
The terms 'q' and 'S' in the lift formula are:	4 risposte
The relationship between induced drag and the aspect ratio is:	4 risposte
The aeroplane drag in straight and level flight is lowest when the:	4 risposte
Which line represents the total drag line of an aeroplane?	4 risposte

Principles of Flight - ATPL - Airline Transport Pilot license Page 31