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Principles of Flight  ATPL  Airline Transport Pilot Licence
ATPL  Airline Transport Pilot Licence
ATPL  Airline Transport Pilot Licence
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The angle of attack (aerodynamic angle of incidence) of an aerofoil is the angle between the:
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The units of wing loading (I) W / S and (II) dynamic pressure q are:
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The angle between the aeroplane longitudinal axis and the chord line is the:
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On a symmetrical aerofoil, the pitching moment for which CL = 0 is:
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Dihedral of the wing is:
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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)
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Which of the following wing planforms produces the lowest induced drag? (all other relevant factors constant)
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The induced drag coefficient, CDi is proportional to:
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If an aeroplane flies in the ground effect
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Which statement is correct about the laminar and turbulent boundary layer:
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ATPL  Airline Transport Pilot Licence
Allenamento!
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