ATPL - Airline Transport Pilot license - Principles of Flight Page 23

Domande Principles of Flight - ATPLPage 23

Critical Mach number is the free stream Mach number at which:	4 risposte
Compared with an oblique shock wave at the same Mach number a normal shock wave has a	4 risposte
The application of the area rule on aeroplane design will decrease the	4 risposte
Vortex generators mounted on the upper wing surface will	4 risposte
When the air is passing through an expansion wave the local speed of sound will	4 risposte
If the sum of all the moments in flight is not zero, the aeroplane will rotate about the:	4 risposte
The value of the manoeuvre stability of an aeroplane is 150 N / g. The stick force required to achieve a load factor of 2.5 from steady level flight is:	4 risposte
Which part of an aeroplane provides the greatest positive contribution to the static longitudinal stability ?	4 risposte
Which phenomenon is counteracted with differential aileron deflection?	4 risposte
An aeroplane has a servo tab controlled elevator. What will happen if the elevator jams during flight?	4 risposte

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