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EN Principles of Flight - ATPL - Airline Transport Pilot license
Questions Principles of Flight - ATPL
The angle of attack (aerodynamic angle of incidence) of an aerofoil is the angle between the:
The units of wing loading (I) W / S and (II) dynamic pressure q are:
The angle between the aeroplane longitudinal axis and the chord line is the:
On a symmetrical aerofoil, the pitching moment for which CL = 0 is:
Dihedral of the wing is:
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)
Which of the following wing planforms produces the lowest induced drag? (all other relevant factors constant)
The induced drag coefficient, CDi is proportional to:
If an aeroplane flies in the ground effect
Which statement is correct about the laminar and turbulent boundary layer:
Other exam subjects ATPL - Airline Transport Pilot license
- Air Law
- Aircraft General Knowledge - Airframe, Systems, Powerplant
- Aircraft General Knowledge - Instrumentation
- Flight Planning and Monitoring
- General Navigation
- Human Performance and Limitations
- IFR Communications
- Mass and Balance
- Meteorology
- Operational Procedures
- Performance
- Radio Navigation
- VFR Communications
