Quiz ATPL | Principles of Flight

The angle of attack (aerodynamic angle of incidence) of an aerofoil is the angle between the:	4 risposte
The units of wing loading (I) W / S and (II) dynamic pressure q are:	4 risposte
The angle between the aeroplane longitudinal axis and the chord line is the:	4 risposte
On a symmetrical aerofoil, the pitching moment for which CL = 0 is:	4 risposte
Dihedral of the wing is:	4 risposte
If the continuity equation is applicable, what will happen to the air density (rho) if the cross sectional area of a tube changes? (low speed, subsonic and incompressible flow)	4 risposte
Which of the following wing planforms produces the lowest induced drag? (all other relevant factors constant)	4 risposte
The induced drag coefficient, CDi is proportional to:	4 risposte
If an aeroplane flies in the ground effect	4 risposte
Which statement is correct about the laminar and turbulent boundary layer:	4 risposte

ATPL - Airline Transport Pilot license - Principles of Flight